DE102022105464A1 - Vehicle with a deployable quantum computer and associated deployable quantum computer system - Google Patents

Abstract

The invention relates to a deployable quantum computer QC and a deployable quantum computer system QUSYS and its applications, in particular in portable devices and vehicles. In contrast to devices from the prior art, the quantum computer QC and thus the quantum computer system QUSYS has means to, firstly, enable mobile operation and, secondly, to reduce interference caused by mobile operation on the quantum computer QC and thus the quantum computer system QUSYS.

Description

Field of invention

The invention is directed to a vehicle with a deployable quantum computer, the corresponding quantum computer and the associated, deployable quantum computer system.

General introduction

Various NP-complete optimization problems arise in vehicles and especially military vehicles. Access to quantum computers with superconducting quantum bits via data connections may be disrupted or disrupted. Then it would no longer be possible to process the corresponding civil and/or military optimization problems.

State of the art

The writing presented here, for example, refers to the writings DE 10 2020 007 977 B4 , DE 10 2020 125 189 A1 , DE 10 2020 101 784 B3 , DE 10 2020 007 977 B4 and to the book Steven Prawer (editor), Igor Aharonovich (editor), “Quantum Information Processing with Diamond: Principles and Applications”, Woodhead Publishing Series in Electronic and Optical Materials, Volume 63, Woodhead Publishing, May 8, 2014, ISBN- 10: 0857096567, ISBN-13: 978-0857096562, the contents of which, to the extent that the legal system of a state in which a subsequent internationalization of this application takes place allows this, are part of the disclosure of the document presented here.

None of these documents clarify the special conditions for mobile use.

Task

The proposal is therefore based on the task of providing a solution for the provision of mobile quantum computers.

This task is solved by an independent claim. Further refinements are the subject of subclaims.

Solution to the task

Quantum computers

This document describes based on the information in the DE 10 2020 101 784 B3 described technical teaching a quantum computer. The document presented here describes a quantum computer with optical readout. Alternatively or in addition to this, the document presented here describes a quantum computer with electrical readout. The quantum computer presented here is based on quantum dots. The quantum dots preferably comprise paramagnetic centers in a substrate. The substrate preferably comprises diamond. The paramagnetic centers preferably include NV centers and/or SiV centers and/or TR1 centers. The quantum computer presented here preferably has an optical device. According to the technical teaching of the document presented here, the optical device is primarily used to irradiate quantum dots and thus the paramagnetic centers with pump radiation. Secondly, the optical device is preferably used to extract fluorescent radiation from the quantum dots. The optical device is therefore preferably used to extract fluorescence radiation from paramagnetic centers. The optical device is therefore preferably used to extract fluorescence radiation from NV centers. An optical functional element of the device is therefore preferably a paramagnetic center in a crystal, in particular an NV center in a diamond crystal and/or a SiV center in a diamond crystal and/or a G center in a silicon crystal or a paramagnetic center in a mixed crystal from elements of the IVth main group of the periodic table. In this context, the document presented here refers to the German patent DE 10 2020 101 784 B3 , whose technical doctrine forms the entirety of this disclosure, to the extent permitted by the law of the state in which nationalization of an international application of the contents of the document presented here takes place.

Such a quantum computer preferably comprises one or more micro-integrated circuits for generating the radio frequency signals, the microwave signals, the direct voltages and drive currents and the control of the light source (LED), which serves as a pump radiation source for resetting the quantum dots of the quantum bits of the relocateable quantum computer.

All of these components of the deployable quantum computer, including the said micro-integrated circuits, are preferably accommodated on the circuit carrier, which can therefore be designed to be particularly compact.

The document presented here reveals a deployable quantum computer. A smartphone or a portable quantum computing system or a vehicle or an autonomous means of transport or a robot or an aircraft or a missile or a rocket or a satellite or a rum missile or a space station or a floating body or a ship or an underwater vehicle or an underwater floating body or a ver A deployable weapon system or another mobile device can, for example, include such a deployable quantum computer. For the sake of simplicity, all of these devices will be referred to as vehicles below. A drive unit for such systems can also include such a deployable quantum computer. Such a drive unit can be an electrostatic or electromagnetic motor or an internal combustion engine or a heat engine or a turbine or a jet engine or a hypersonic engine or a rocket engine or a plasma engine or an engine with a magnetic field for confining a plasma, such as from the Vasimir project known. (See for example: Franklin R. Chang Diaz, F. Wall y Baitty, Jared P. Squire, Richard H. Goulding, Edgar A. Bering, Roger D. Bengtson, “The Vasimr Engine: Project Status and Recent Accomplishments,” downloadable on January 9, 2022 from https://ntrs.nasa.gov/api/citations/20110011201/downloads/20110011201.pdf.) In the sense of the document presented here, deployability means that the claimed device is suitable and designed to do so in a short time to be moved from a first location to a second location and to be operated both at the first location and at the second location and/or during the movement from the first location to the second location. Here, short time is typically a time shorter than a day, better shorter than 12 hours, better shorter than 6 hours, better shorter than 2 hours, better than 1 hour, better shorter than 30 minutes, better shorter than 15 minutes, better shorter than 5 minutes, better shorter than 2 minutes, better understood as shorter than 1 minute. The time for moving the device from a first location to a second location can also be 0s if the device is ready for use almost immediately from the user's perspective and/or is permanently ready for use and, for example, simply moves, i.e. remains usable, for example, during the movement. Readiness for use in the sense of the document presented here means being ready for intended use.

The document presented here proposes a deployable quantum computer QC in a mobile device. How the document presented here understands the term mobile device is described above. The core of the quantum computer QC forms a substrate D. The substrate D preferably has one or more quantum dots NV1, NV2, NV3. Their nature will be explained in more detail below. In this context, the document presented here also expressly refers to Scripture DE 10 2020 007 977 B4 , the content of which is a full part of the disclosure content of the document presented here, insofar as the legal system of the state in which the nationalization takes place allows this in the event of a later nationalization of a later international application.

Furthermore, the deployable quantum computer QC presented here preferably includes a light source LD and an associated light source driver LDRV. In order to be able to influence the quantum state of the quantum dots NV1, NV2, NV3, the proposed deployable quantum computer QC preferably has one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3. The deployable quantum computer QC preferably comprises a control device μC. The control device μC preferably controls the light source driver LDRV and thus the emission of pump radiation LB with the pump radiation wavelength λ _pmp . The control device μC preferably also controls the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3. The control device µC preferably has a memory one or more RAM, NVM. the control device µC for program commands and data. The proposed quantum computer QC preferably comprises a waveform generator WFG for controlling the light source driver LDRV by means of a transmission signal S5. The control device µC preferably also controls the waveform generator WFG. The proposed quantum computer QC preferably also includes an optical system OS for irradiating the quantum dots NV1, NV2, NV3 in the substrate D with the pump radiation LB from the light source LD. Furthermore, the proposed deployable quantum computer QC preferably comprises an optical and/or electronic quantum state readout device for reading out the current quantum states of the quantum dots NV1, NV2, NV3. In the case of an optical quantum state readout device, the quantum state readout device preferably comprises a photodetector PD and an amplifier V. In the case of an electrical quantum state readout device, the quantum state readout device preferably comprises contacts for contacting the substrate D and a voltage source for generating an extraction voltage between such contacts of the substrate D and an amplifier V Amplification of the photocurrent extracted in this way of the quantum dots NV1, NV2, NV3. The amplifier V can include a transimpedance amplifier as an internal amplifier IVV. In this case, the quantum state reading device comprises a device for electronically reading out the states of the quantum dots NV1, NV2, NV3. The quantum dots NV1, NV2, NV3 are preferably located in the substrate D. The substrate D is preferably doped in the area of the quantum dots NV1, NV2, NV3. This doping preferably shifts the Fermi level in the area of the quantum dots NV1, NV2, NV3 in such a way that the quantum dots NV1, NV2, NV3 are electrically charged. The substrate D is preferred Area of quantum dots NV1, NV2, NV3 n-doped. This n-doping preferably shifts the Fermi level in the area of the quantum dots NV1, NV2, NV3 in such a way that the quantum dots NV1, NV2, NV3 are negatively electrically charged. Typically, the waveform generator WFG generates a light source control signal S5, typically depending on settings of the control device µC. The light source driver LDRV preferably supplies the light source LD with electrical energy depending on the light source control signal S5 and possibly typically depending on the settings of the control device μC. The control device µC typically controls the waveform generator WFG. The light source LD at least temporarily irradiates the quantum dot or the multiple quantum dots NV1, NV2, NV3 using the optical system OS with pump radiation LB of the pump radiation wavelength λ _pmp . The one or more quantum dots NV1, NV2, NV3 emit fluorescence radiation FL with a fluorescence radiation wavelength λ _fl , as a result of the irradiation with electromagnetic radiation of the pump radiation wavelength λ _pmp . In the case of optical reading of the quantum states of the quantum dots NV1, NV2, NV3, the photodetector PD detects at least part of the fluorescence radiation FL by means of the optical system OS. In this case, the photodetector PD converts at least part of the fluorescence radiation FL into a receiver output signal S0. A subsequent amplifier V amplifies and, if necessary, filters the receiver output signal S0 into a received signal S1. In the case of electronic reading of the quantum states of the quantum dots NV1, NV2, NV3, the device for electronically reading out the states of the quantum dots NV1, NV2, NV3 generates the received signal S1. The control device µC controls the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3. The control device µC can be used to control one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or by controlling the emission of the light source LD states of the quantum dots NV1, Change NV2, NV3. The control device µC can be used to control one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or by controlling the emission of the light source LD states of the quantum dots NV1 , NV2, NV3 link together. For this purpose, the control device μC typically has means for generating a measured value signal S4 with one or more measured values from one or more received signals S1. The measured value signal S4 depends on quantum states of quantum dots NV1, NV2, NV3. What is special about the quantum computer QC is that, in contrast to the prior art, the deployable quantum computer QC and/or the mobile device has a deployable power supply (LDV, TS, BENG, SRG) for supplying at least some of the sub-devices of the quantum computer QC with energy. The relocatable energy supply (LDV, TS, BENG, SRG) preferably has a mobile energy supply (LDV, TS, BENG) and an energy processing device SRG, in particular a voltage converter or a voltage regulator or a current regulator.

A further embodiment of the deployable quantum computer QC preferably has not only quantum dots NV1, NV2, NV3, but also one or more nuclear core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . In this case, the proposed deployable quantum computer QC preferably also has one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 1 , _{CI2 2 ,} CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ on. Typically, the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are entirely or at least partially identical to the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3, which then at the same time also have one or more devices for generating an electromagnetic wave field at respective locations of the core quantum dots CI1 ₂ , C11 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are. The quantum dots NV1, NV2, NV3 and the nuclear core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are preferably located in the common substrate D. Control device μC controls one or the other several devices mWA, MW/RF-AWFG to generate an electromagnetic wave field. The control device µC can then control the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by controlling the emission of the light source LD, quantum states of the quantum dots NV1, NV2, NV3 and/or quantum states of the core quantum dots CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ change. The control device µC can then couple quantum dots NV1, NV2, NV3 with other quantum dots NV1, NV2, NV3 by controlling one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by controlling the emission of the light source LD The control device µC can then control one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by controlling the emission of the light source LD, quantum dots NV1, NV2, NV3 with core quantum dots CI1 ₁ , CI1 ₂ , Pair CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The control device µC can then control one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field and/or by controlling the emission of the light source LD core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ with other core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 1 , CI3 ₂ , CI3 _{3 .} The measured value signal S4 depends on quantum states of quantum dots NV1, NV2, NV3 and/or on states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

In a further detail of the deployable quantum computer QC, the mobile energy supply (LDV, TS, BENG) supplies the energy processing device SRG with energy, the energy processing device SRG in turn supplying other device parts of the deployable quantum computer QC with electrical energy.

In a more specific variant, the mobile energy supply (LDV, TS, BENG) includes a charging device LDV and a disconnecting device TS and an energy reserve BENG. This enables an improvement in the EMC sensitivity of the deployable quantum computer QC. (EMC = electromagnetic compatibility). For this purpose, the proposed deployable quantum computer QC preferably has a first operating mode and a second operating mode. In the first operating mode of the deployable quantum computer QC, the separating device TS first connects the charging device LDV with the energy reserve BENG, so that the charging device LDV charges the energy reserve BENG with electrical energy from an external energy supply PWR in this first operating mode. In the first operating mode, firstly, the separating device TS connects the charging device LDV to the energy processing device SRG and secondly, the charging device LDV supplies the energy processing device SRG with electrical energy from the external energy supply PWR. In the second operating mode, firstly the separating device TS preferably separates the charging device LDV from the energy reserve BENG and secondly the separating device TS separates the charging device LDV from the energy processing device SRG. Thirdly, in the second operating mode, the energy reserve BENG preferably supplies the energy processing device SRG with electrical energy.

In a further embodiment, the deployable quantum computer QC includes a housing GH and a shield AS. Preferably there are the light source LD and the light source driver LDRV and the substrate D and the devices mWA, MW/RF-AWFG for generating the electromagnetic wave field and the control device µC and the memory RAM, NVM of the control device µC and the optical system OS and if necessary. the amplifier V and the shield AS are inside the housing GH. This protects these device parts and possibly the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 _{1 , CI2 2 ,} CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in the substrate D from disruptive EMC influences . Typically, the shield AS can be part of the housing GH or the housing GH itself. Preferably there are at least parts of the device parts of the energy supply (LDV, TS, BENG, SRG) of the deployable quantum computer QC or those parts of the energy supply (LDV, TS, BENG, SRG) of the deployable quantum computer QC that provide an autonomous energy supply for a certain time enable autonomous operation of the deployable quantum computer QC, located within the common housing GH. The parts preferably have their own shielding AS.

An energy processing device SRG and an energy reserve BENG of the energy supply (LDV, TS, BENG, SRG) of the quantum computer QC are preferably located within the shield AS.

So that the relocatable quantum computer QC can be operated as a mobile quantum computer QC even during relocation, the relocatable quantum computer QC includes means for its operation, the relocatable quantum computer QC and all the necessary means for operating this relocatable quantum computer QC being part of a mobile device. To make this possible, these means for operating the deployable quantum computer QC are typically also deployable. For the same reason, these means for operating the deployable quantum computer QC are preferably part of the deployable quantum computer QC. Both the deployable quantum computer QC and these means for operating the deployable quantum computer QC are preferably part of the mobile device. It is typically irrelevant whether the operation of the deployable quantum computer QC is coupled to means and/or commands from outside the deployable quantum computer QC despite the presence of all means for operating the deployable quantum computer QC as part of the deployable quantum computer QC.

As already mentioned above, the deployable quantum computer QC is often part of a mobile device, the mobile device in particular being a smartphone or a portable quantum computer system or a vehicle or a robot or an aircraft or a missile or a satellite or a rum missile or a space station or a Floating body or a ship or an underwater vehicle or an underwater floating body or a deployable weapon system or another mobile device.

In a further embodiment, the deployable quantum computer QC preferably comprises a positioning device XT, YT. The positioning device XT, YT can preferably position the substrate D relative to the optical system OS in such a way that the optical system OS, in cooperation with the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field, is first in a first positioning can control a first set of quantum dots with a first number of quantum dots and possibly a second number of core quantum dots and secondly in a second positioning can control a second set of quantum dots with a third number of quantum dots and possibly a fourth number of core quantum dots. The control device μC preferably controls the positioning device XT, YT for the substrate D in such a way that it assumes the first positioning or the second positioning or further positioning. In this way, the deployable quantum computer QC can always reconfigure itself depending on its operating temperature during operation and/or during breaks in operation so that it can always use a maximum of quantum dots and core quantum dots.

In a further refinement, the deployable quantum computer QC therefore has a temperature sensor ST, which determines a temperature measurement value for the temperature of the substrate D or for the temperature of a sub-device of the deployable quantum computer QC that is thermally connected to it.

This results in a version of the deployable quantum computer QC, wherein the deployable quantum computer QC is set up and intended to work with a reduced first number of quantum dots even at room temperature of the substrate D or a temperature measurement value that corresponds to a value greater than 0 ° C can. At the same time, however, the deployable quantum computer QC is also set up and intended to be able to work with an increased, third number of quantum dots at a temperature measurement value that corresponds to a value less than 0 ° C. In this way, the deployable quantum computer QC can always reconfigure itself depending on its operating temperature during operation and/or during breaks in operation so that it can always use a maximum of quantum dots and core quantum dots.

The document presented here therefore discloses in one form a deployable quantum computer QC, which is set up and intended to work with a reduced second number of core quantum dots even at room temperature of the substrate D or a temperature measurement value that corresponds to a value greater than 0 ° C can. Preferably, the deployable quantum computer QC is simultaneously set up and intended to be able to work with an increased fourth number of core quantum dots at a temperature measurement value that corresponds to a value less than 0 ° C. In this way, the deployable quantum computer QC can always reconfigure itself depending on its operating temperature during operation and/or during breaks in operation so that it can always use a maximum of quantum dots and core quantum dots.

In a further embodiment, the deployable quantum computer QC has one or more deployable cooling devices KV, which can be deployed together with the deployable quantum computer (QC). One or more of the deployable cooling devices KV are preferably suitable and/or intended to control the spin temperature of quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or to lower the temperature of the substrate D.

In a further embodiment, one or more such cooling devices KV lower the temperature of quantum dots NV1, NV2, NV3 and/or the temperature of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or the temperature of the substrate D to such an extent that the deployable quantum computer QC can work with a third number of quantum dots NV1, NV2, NV3 that is increased compared to the reduced first number of quantum dots NV1, NV2, NV3. One or more such cooling devices KV preferably lower the temperature of quantum dots NV1, NV2, NV3 and/or the temperature of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or the temperature of the substrate D to such an extent that the quantum computer QC has a reduced second number of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ an increased fourth number of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ can work.

In a further embodiment, one or more of the relocatable cooling devices KV of the quantum computer QC include one or more closed loop helium gas cooling systems HeCLCS or one or more relocatable closed loop helium gas cooling systems HeCLCS include one or more relocatable cooling devices KV.

In a further embodiment, the deployable quantum computer QC includes a deployable second deployable energy supply BENG2, which is different from the first deployable energy supply BENG. The second relocatable energy supply BENG2 preferably supplies one or more of the relocatable cooling devices KV and/or one or more of the closed loop helium gas cooling systems HeCLCS with energy.

In another embodiment, the deployable quantum computer QC and/or the mobile device have a mobile data interface DBIF, in particular a mobile radio data interface and/or a wired data interface.

Preferably, by means of this data interface DBIF, in a further embodiment, a higher-level computer system, for example a central control device ZSE, can control the control device µC in such a way that the control device µC of the deployable quantum computer QC can use the deployable quantum computer QC to carry out at least one manipulation of a state of at least one quantum bit of the quantum bits NV1, NV2, NV3 and/or to carry out at least one manipulation of a state of at least one nuclear core quantum bit of the nuclear core quantum bits CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The higher-level central control unit ZSE preferably controls the control device μC via the mobile data interface DBIF.

The first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 preferably comprise one or more batteries and/or one or more accumulators or one or more capacitors and/or one or more interconnection of several of these energy storage devices. The deployable quantum computer QC and/or the mobile device preferably have one or more charging devices LDV. Typically, one or more charging devices LDV are intended and/or are intended to store energy at least temporarily in at least some or all of the rechargeable energy storage devices BENG, BENG2.

In a variant, in the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 can comprise one or more energy stores that generate energy from at least one or more fluids by means of chemical and/or electrochemical processes. In this case, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 and/or the quantum computer QC preferably have one or more storage tanks for these fluids. One or more of these storage tanks supply one or more energy storage devices of the quantum computer QC with one or more of these fluids, which typically serve to generate energy. Preferably, one or more of the energy storage devices include one or more galvanic cells and/or one or more fuel cells and/or one or more internal combustion engines and/or turbines and the like, each of which is coupled to one or more electrical generators, and/or one or a plurality of thermal energy conversion machines, each coupled to one or more electrical generators. One or more of the mobile energy supplies of the quantum computer QC preferably have one or more energy processing devices SRG, in particular one or more voltage converters and/or one or more voltage regulators and/or one or more current regulators. One or more of the energy storage devices preferably supply the energy processing devices SRG with energy. One or more of the energy processing devices SRG preferably in turn supply one or more device parts of the quantum computer QC with electrical energy that has been suitably prepared and stabilized for the relevant device part.

In a further variant of the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy stores that generate energy using mechanical processes. One or more of these energy stores then preferably comprise one or more generators and/or one or more alternators and/or one or more electric motors that can be operated as a generator. Typically, one or more mobile energy supplies of the quantum computer QC have one or more energy processing devices SRG, in particular one or more voltage converters or one or more voltage regulators or one or more current regulators. One or more of the energy storage devices supply one or more of the energy processing devices SRG with energy. One or more of the energy processing devices SRG then preferably supply one or more other device parts of the deployable quantum computer QC with electrical energy.

In a further variant of the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 preferably comprise one or more energy storage devices that generate energy by converting electromagnetic radiation, in particular light, into electrical energy. For this purpose, one or more of the energy storage devices preferably include one or more solar cells and/or one or more functionally equivalent devices, such as PN junctions. In this case, one or more of the mobile energy supplies of the quantum computer QC preferably have one or more energy processing devices SRG, in particular one or more voltage converters and/or one or more voltage regulators and/or one or more current regulators. One or more of the energy stores of the energy reserve BENG, BENG2 of the quantum computer QC then typically supply one or more of the energy processing devices SRG with energy at least temporarily. One or more energy processing devices SRG then supply one or more other device parts of the quantum computer QC with electrical energy.

In a further variant of the deployable quantum computer QC, the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy storage devices that generate energy using nuclear processes. One or more of the mobile energy supplies of the quantum computer QC include one or more energy processing devices SRG, in particular one or more voltage converters and/or one or more voltage regulators and/or one or more current regulators. One or more of the energy stores of the energy reserve BENG, BENG2 of the quantum computer QC preferably supply one or more of the energy processing devices SRG with energy at least temporarily. One or more of these energy processing devices SRG then in turn supply one or more device parts of the deployable quantum computer QC with electrical energy.

In a further embodiment, one or more of the energy storage devices comprise one or more thermonuclear batteries or radionuclear batteries or one or more devices that are functionally equivalent to such a thermonuclear battery.

In a further variant, the substrate D comprises diamond. In this case, one or more of the quantum dots NV1, NV2, NV3 in the substrate D are preferably defect centers and/or paramagnetic centers in diamond. One or more of the defect centers in diamond NV centers or ST1 centers or SiV centers or TR12 centers are then particularly preferred.

The deployable quantum computer QC preferably comprises one or more core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ based on isotopes with a magnetic moment μ. The core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ are preferably coupled to quantum dots NV1, NV2, NV3.

Preferably, the substrate D is essentially isotopically pure, at least in regions in the area of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and the quantum dots NV1, NV2, NV3. This has the advantage that the magnetic moments of the core quantum dots CI1 ₁ , CI1 ₂ , C1I ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and the quantum dots NV1, NV2, NV3 do not have such parasitic magnetic moments of impurities in the substrate D. For this purpose, the isotopes of the substrate D, apart from atoms that form the core quantum dots CI1 ₁ , CI12, CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ , preferably essentially no magnetic nuclear moment.

In a further embodiment, the deployable quantum computer QC has one or more fans and/or one or more heat exchangers for heat exchange with the environment and/or one or more heat exchangers for heat exchange with the ambient air and/or one or more radiation coolers for heat exchange with the ambient air or the environment by means of electromagnetic heat radiation.

In a further variant of the deployable quantum computer QC, one or more of the fans and/or one or more of the heat exchangers exchange energy in the form of heat with one or more of the deployable cooling devices KV.

In a further modification, the deployable quantum computer QC has an internal shielding AS. The internal shielding AS preferably shields the substrate D with the quantum dots NV1, NV2, NV3 and possibly the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ against electromagnetic Fields of the control device µC and / or the memory RAM, NVM and / or the power supply SRG, TS, LDV, BENG, BENG2 and / or the light source driver LDRV and / or the light source LD. In a further modification, the deployable quantum computer QC has an internal shielding AS. The internal shielding AS preferably shields the substrate D with the quantum dots NV1, NV2, NV3 and possibly the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ against magnetic fields the control device µC and/or the memory RAM, NVM and/or the power supply SRG, TS, LDV, BENG, BENG2 and/or the light source driver LDRV and/or the light source LD.

In order to be able to relocate the relocatable quantum computer QC, the relocatable quantum computer QC is in this case preferably equipped, at least temporarily, with one or more wheels or a chassis or functionally equivalent device parts, which can also be driven and / or braked.

In another embodiment, the deployable quantum computer QC has, at least at times, one or more drive devices. According to the proposal, one or more of the drive devices is a wheel or a propeller or a propeller or a turbine or a rocket engine or a drive wheel or an MHD engine. MHD stands for magnetohydrodynamic.

In embodiments of the deployable quantum computer QC, which are to be operated in a fluid and moved for deployment, it is expedient if, in certain applications, such a deployable quantum computer QC has aerodynamically and/or hydrodynamically shaped functional elements for reducing and/or controlling aerodynamic effects and/or hydrodynamic Effects and / or for generating dynamic buoyancy, in particular wings and / or flaps.

• - die Steuervorrichtung µC und/oder
• - der Speicher RAM, NVM der Steuervorrichtung µC und/oder
• - der Rechnerkern CPU und/oder
• - die Datenschnittstelle DBIF und/oder
• - die interne Datenschnittstelle MDBIF und/oder
• - der Lichtquellentreiber LDRV und/oder
• - der Wellenformgenerator WFG und/oder
• - der Verstärker V und/oder
• - der Fotodetektor PD und/oder
• - die erste Kameraschnittstelle CIF und/oder
• - die zweite Kameraschnittstelle CIF2 und/oder
• - die erste Kamera CM1 und/oder
• - die zweite Kamera CM2 und/oder
• - der Temperatursensor ST und/oder
• - der Mikrowellen- und/oder Radiowellenfrequenzgenerator MW/RF-AWFG zur Erzeugung weitestgehend frei vorgebbarer Wellenformen und/oder
• - die Magnetfeldsensoren MSx, MSy, MSz und /oder
• - die Magnetfeldsteuerungen MFSx, MFSy, MFSz und/oder
• - die erste Energieaufbereitungsvorrichtung SRG und/oder
• - die zweite Energieaufbereitungsvorrichtung SRG2 und/oder
• - die Energiereserve BENG und/oder
• - die zweite Energiereserve BENG2 und/oder
• - die Trennvorrichtung TS und/oder
• - die Ladevorrichtung LDV.

In some special versions of the deployable quantum computer QC, it makes sense for electronic device parts of the quantum computer QC to be at least partially designed in radiation-hard electronics. Such preferably radiation-hard device parts of the quantum computer QC are, for example:

• - the control device µC and/or
• - the memory RAM, NVM of the control device µC and/or
• - the computer core CPU and/or
• - the data interface DBIF and/or
• - the internal data interface MDBIF and/or
• - the light source driver LDRV and/or
• - the waveform generator WFG and/or
• - the amplifier V and/or
• - the photodetector PD and/or
• - the first camera interface CIF and/or
• - the second camera interface CIF2 and/or
• - the first camera CM1 and/or
• - the second camera CM2 and/or
• - the temperature sensor ST and/or
• - the microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms and/or
• - the magnetic field sensors MSx, MSy, MSz and/or
• - the magnetic field controls MFSx, MFSy, MFSz and/or
• - the first energy processing device SRG and/or
• - the second energy processing device SRG2 and/or
• - the energy reserve BENG and/or
• - the second energy reserve BENG2 and/or
• - the separating device TS and/or
• - the LDV loading device.

In the sense of the document presented here, radiation-hard means that these functional elements of the quantum computer QC are intended and/or suitable for use in space and/or in areas of increased ionizing radiation, such as nuclear reactors or the environment of thermonuclear batteries.

In many applications, it is advantageous if the deployable quantum computer QC has a control device μC, which at least temporarily executes a neural network model. The neural network model that the control device µC typically executes processes input values and/or the values of input signals. The neural network model that the control device µC typically executes outputs output signals and/or output values of output signals. The control device µC then preferably influences states of quantum dots NV1, NV2, NV3 and/or states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ as a function of output signals and/or output values of the neural network model that the control device µC typically executes , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . Conversely, the control device preferably influences μC depending on states of quantum dots NV1, NV2, NV3 and/or states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ A input signals and/or input values of the neural network model that the control device µC typically executes.

Thus, the document presented here discloses, among other things, a smartphone and/or a portable quantum computer system and/or a mobile quantum computer system and/or vehicle and/or robot and/or aircraft and/or missile and/or satellite and/or a rum missile and/or space station and/or floating body and/or ship and/or underwater vehicle and/or surface floating body and/or underwater floating body and/or deployable weapon system and/or warhead and/or surface or underwater vehicle and/or projectile and/or other mobile device and/or movable Contraption. For the sake of simplicity, the document presented here refers to all of these as “vehicles”. The document presented here therefore proposes a vehicle in this very broad sense, which includes a deployable quantum computer QC, as described above. Conversely, the document presented here proposes a deployable quantum computer as previously described, which is a vehicle in the broad sense described above.

In a further, preferred variant, the quantum computer QC is intended to decrypt and/or encrypt the data communication, in particular of the control device μC, via a data interface DBIF. This is preferably the data interface DBIF of the control device µC.

Such a vehicle preferably includes sensors and/or measuring means in the broadest sense, which transmit measured values about the surroundings of the vehicle and/or conditions of the vehicle and/or conditions of the vehicle occupants or users of the vehicle and/or conditions of the vehicle's payload to the Supply control device µC. Under certain circumstances, the control device µC also receives measured values about the vehicle's surroundings via the DBIF data interface. The quantum computer QC and possibly the control device μC can preferably determine a situation assessment for the overall condition of the vehicle and/or the surroundings of the vehicle depending on such measured values. The overall condition of the vehicle in the sense of the document presented here can include the condition of the vehicle's surroundings and/or the condition of the vehicle occupants and/or the condition of the vehicle's load.

• - ein Radar-Sensor und/oder
• - ein Mikrofon und/oder
• - ein Ultraschalmikrofon und/oder
• - ein Infraschallmikrofon und/oder
• - einen Ultraschalltransducer und/oder
• - einen Infrarotsensor und/oder
• - einen Gassensor und/oder
• - einen Beschleunigungssensor und/oder
• - ein Geschwindiglkeitssensor und/oder
• - einen Strahlungsdetektor und/oder
• - ein bildgebendes System und/oder
• - eine Kamera und/oder
• - eine Infrarotkamera und/oder
• - eine Multisprektralkamera und/oder
• - ein LIDAR-System und/oder
• - ein Ultraschallmesssystem und/oder
• - ein Dopplerradarsystem und/oder
• - ein Quantenradarsystem und/oder
• - ein Quantensensor und/oder
• - ein Positionssensor und/oder
• - ein Navigationssystem und/oder
• - ein GPS-Sensor (oder eine funktionsäquivalente Vorrichtung) und/oder
• - ein Lagesensor und/oder
• - ein Partikelzähler und/oder
• - ein Detektionssystem für biologische Stoffe, insbesondere für biologische Kampstoffe, und/oder
• - ein Gravimeter und/oder
• - ein Kompass und/oder
• - ein Gyroskop und/oder
• - ein MEMS-Sensor und/oder
• - ein Drucksensor und/oder
• - ein Neigungswinkelsensor und/oder
• - ein Temperatursensor und/oder
• - ein Feuchtesensor und/oder
• - ein Windgeschwindigkeitssensor und/oder
• - ein Wellenfrontsensor und/oder
• - ein mikrofluidisches Messsystem und/oder
• - ein Abstandsmesssystem und/oder
• - ein Längenmesssystem und/oder
• - ein biologischer Sensor zur Detektion biologischer Marker und/oder Viren und/oder Mikroben oder dergleichen und/oder
• - ein Sensorsystem zur Erfassung biologischer Messwerte von Fahrzeuginsassen und/oder zur Erfassung biologischer Messwerte lebender Ladung, insbesondere von Tieren und/oder biologischen Materialien,
• - ein Seat-Occupation-Messystem und/oder
• - ein Spannungssensor und/oder ein Stromsensor und/oder ein Leistungssensor.

In a further form, the document presented here proposes that at least one or more sensors SENS of the vehicle is one of the following sensors SENS that deliver measured values or that it includes at least one of the following sensors SENS that deliver measured values as a subsystem:

• - a radar sensor and/or
• - a microphone and/or
• - an ultrasound microphone and/or
• - an infrasonic microphone and/or
• - an ultrasound transducer and/or
• - an infrared sensor and/or
• - a gas sensor and/or
• - an acceleration sensor and/or
• - a speed sensor and/or
• - a radiation detector and/or
• - an imaging system and/or
• - a camera and/or
• - an infrared camera and/or
• - a multispectral camera and/or
• - a LIDAR system and/or
• - an ultrasound measuring system and/or
• - a Doppler radar system and/or
• - a quantum radar system and/or
• - a quantum sensor and/or
• - a position sensor and/or
• - a navigation system and/or
• - a GPS sensor (or a functionally equivalent device) and/or
• - a position sensor and/or
• - a particle counter and/or
• - a detection system for biological substances, in particular for biological agents, and/or
• - a gravimeter and/or
• - a compass and/or
• - a gyroscope and/or
• - a MEMS sensor and/or
• - a pressure sensor and/or
• - an inclination angle sensor and/or
• - a temperature sensor and/or
• - a humidity sensor and/or
• - a wind speed sensor and/or
• - a wavefront sensor and/or
• - a microfluidic measuring system and/or
• - a distance measuring system and/or
• - a length measuring system and/or
• - a biological sensor for detecting biological markers and/or viruses and/or microbes or the like and/or
• - a sensor system for recording biological measurements of vehicle occupants and/or for recording biological measurements of living cargo, in particular of animals and/or biological materials,
• - a seat occupation measurement system and/or
• - a voltage sensor and/or a current sensor and/or a power sensor.

As a consistent further development, the document presented here proposes a vehicle in the broad sense described above, in which the quantum computer QC controls the vehicle and/or device parts of the vehicle and/or influences a control of the vehicle or a device part of the vehicle depending on these measured values .

The document presented here further proposes a variant in which the vehicle has an interior and in which the quantum computer QC influences parameters of the interior of the vehicle and/or a device part in the interior of the vehicle depending on the measured values.

The technical teaching presented here reveals in particular that the vehicle can be a weapon system and/or that the vehicle can include a weapon system that is coupled to the quantum computer QC.

For military applications, the vehicle may include a fire control system. The fire control system can in turn comprise one or more quantum computers QC and/or be coupled to one or more quantum computers QC. The control of the weapon system by the fire control system preferably depends, at least temporarily, on the quantum computer QC and its signaling. The weapon system is controlled by the fire control system preferably in interaction between the fire control system and the QC quantum computer.

The vehicle preferably comprises an evaluation device which classifies the intended control of the weapon system with regard to the expected effects before the control is carried out and determines a control command class. The evaluation device preferably prevents execution of the control or postpones this execution until it is released by a human user if the control command determined in cooperation with the quantum computer QC falls into a predetermined control class.

The vehicle can, for example, identify one or more targets with the help of the deployable quantum computer QC.

The vehicle can then, for example, classify the one or more targets with the help of the deployable quantum computer QC, in particular with the aid of a neural network program, which can be executed, for example, by a control computer µC of the deployable quantum computer QC.

In the case of a vehicle for military purposes or a weapon system, the vehicle or weapon system can use the QC quantum computer to determine a temporal order or prioritization of the combat against multiple targets.

In the case of a vehicle for military purposes or a weapon system, the vehicle or weapon system can use the QC quantum computer to determine a time to engage a target.

In the case of a vehicle for military purposes or a weapon system, the vehicle or the weapon system can use the QC quantum computer to determine a weapon type and/or ammunition to combat a target.

The document presented here suggests, among other things, a possible version of a vehicle that uses the quantum computer QC to determine a route for the vehicle.

In the case of a vehicle for military purposes or a weapon system, the vehicle or weapon system can use the quantum computer QC to determine a route for a weapon or a warhead or a projectile or an ammunition or another vehicle.

The document presented here also proposes, among other things, a vehicle in which the control device μC at least temporarily executes a neural network model and in which the neural network model processes input values and/or input signals and outputs output signals and/or output values. As already described above, the control device µC typically influences states of the quantum dots NV1, NV2, NV3 and/or states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ depending on output signals and/or output values of the neural network model , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .Typical In this embodiment, the control device influences μC depending on the states of the quantum dots NV1, NV2, NV3 and/or states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ input signals and/or input values of the neural network model.

Substrate

As described above, the deployable quantum computer QC according to the proposal comprises a substrate D with one or more quantum dots NV1, NV2, NV3. The substrate D preferably comprises diamond as the substrate material. The diamond is preferably isotopically pure or has at least one isotopically pure portion, which preferably has the quantum dots NV1, NV2, NV3. The quantum dots NV1, NV2, NV3 are preferably paramagnetic centers. In the case when the substrate material of the material of the substrate D comprises diamond, the paramagnetic centers are preferably ST1 centers and/or preferably TR1 centers and/or very particularly preferably NV centers. This means that interference caused by such isotopic impurities does not interfere with the functionality of the quantum bits, or at most only does so to a sufficiently small extent. In relation to diamond, this means that the diamond preferably consists essentially of ¹² C isotopes as base isotopes. Such ¹² C isotopes do not have a magnetic moment that can interact with the quantum dots NV1, NV2, NV3. The core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are preferably also located in the isotopically pure region of the substrate D. When we talk about isotope purity here, they are Isotopes that serve as core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are not taken into account when assessing the isotope purity. At this point, this writing specifically refers to Scripture DE 10 2020 125 189 A1 , whose technical teachings for the following international procedures, to the extent legally permissible in the relevant registration countries, are part of the disclosure of this document by reference. Isotopes purely within the meaning of this disclosure and the DE 10 2020 125 189 A1 is a material when the concentration of isotopes other than the base isotopes that dominate the material is so low that the technical purpose is achieved to a level sufficient for the production and sale of products with an economically sufficient production yield. The DE 10 2020 125 189 A1 lists the relevant isotope ratios of the relevant elements on which the technical teaching disclosed here is based. Since isotopically pure diamonds are extremely expensive, it makes sense if the substrate D comprises a diamond material and, for example, the diamond material comprises an epitaxially at least locally grown isotopically pure layer essentially made of ¹² C isotopes. This can be deposited, for example, using CVD and other deposition methods on the original surface of a silicon wafer used as substrate D or a diamond surface. From now on, the term substrate D includes the part of the combination of substrate D and epitaxially grown layer DEPI in which the quantum dots NV1, NV2, NV3 are manufactured. Typically this is the epitaxial layer DEPI. Essentially this means that the total proportion K _1G ' of the C isotopes with magnetic moment, which are part of the substrate D, based on 100% of the C atoms, which are part of the substrate D, compared to those in the tables of DE 10 2020 125 189 A1 specified natural total proportion K _1G is reduced to a proportion K _1G 'of the C isotopes with magnetic moment which are part of the substrate D, based on 100% of the C isotopes which are part of the substrate D. This proportion K _1G ' is preferably smaller than 50%, better smaller than 20%, better smaller than 10%, better smaller than 5%, better smaller than 2%, better smaller than 1%, better smaller than 0.5% , better less than 0.2%, better less than 0.1% of the natural total proportion K _1G for C isotopes with magnetic moment on the C isotopes of the substrate D in the area of influence of the quantum dots NV1, NV2, NV3 and/or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . When determining the proportion K _{1G ', those C atoms of the core quantum dots CI1 1 ,} CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ not taken into account because their magnetic moments are intentional and therefore not parasitic.

The use of NV centers and/or ST1 centers and/or TR12 centers or L1 centers as quantum dots NV1, NV2, NV3 of the quantum bits of the quantum computer enables the QC quantum computer to be operated at room temperature and thus enables the quantum computer to be deployed in the first place QC. The electron spin configuration of such a paramagnetic center serves as a quantum dot of the quantum dots NV1, NV2, NV3. In addition to such quantum dots NV1, NV2, NV3 as quantum bits, the deployable quantum computer QC preferably also includes nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ as nuclear core quantum bits. Typically, the magnetic moments of isotopes that have non-zero magnetic moments due to nuclear spin serve as nuclear nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . Such nuclear magnetic moments of the relevant isotopes of the nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ preferably couple with the electron configuration of the paramagnetic centers of the Quan ten points NV1, NV2, NV3. This allows a control device μC of the quantum computer QC to manipulate the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ by manipulating the states of the quantum dots NV1, NV2, NV3 . The control device μC can also read the nuclear quantum states of the nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ by electrically or optically reading out the quantum states of the quantum dots NV1, NV2 , Capture NV3. The control device µC can also couple core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ that are distant from one another by means of chains of coupled quantum dots NV1, NV2, NV3. The nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ thus form nuclear core quantum bits. These nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 _{1 , CI2 2 ,} CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are preferably the nuclear spins of isotopes with a magnetic nuclear nuclear moment. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 , whose technical teachings for the following international procedures, to the extent legally permissible in the relevant registration countries, are part of the disclosure of this document by reference. The nuclear quantum dots CI1 ₁ , CI1 _{2 ,} CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the nuclear quantum bits are characterized by very long T2 times. The proposed deployable quantum computer QC preferably uses its quantum dots NV1, NV2, NV3 to control and entangle the states of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and for reading out the nuclear quantum states of the nuclear quantum dots CI1 ₁ , CI1 ₂ , C11 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ . The quantum states of the quantum dots NV1, NV2, NV3 can be read out optically and/or electrically. With regard to electrical reading, this document expressly refers to the document DE 10 2020 125 189 A1 , whose technical teachings for the following international procedures, to the extent legally permissible in the relevant registration countries, are part of the disclosure of the document presented here by reference. Another advantage of the deployable quantum computer QC proposed here is the relatively easy operation and the better selectivity of the control of the quantum dots NV1, NV2, NV3 and the quantum bits and the good scalability compared to other quantum computers.

As described above, a proposed quantum computer QC typically comprises a substrate D with one or more quantum dots NV1, NV2, NV3. In addition, the substrate D preferably also has one or more nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 _{1 , CI3 2 ,} CI3 ₃ . The quantum dots NV1, NV2, NV3 are preferably one or more paramagnetic centers which form one or more quantum bits. Preferably, the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are one or more isotopes with a magnetic moment, which form one or more core quantum bits. The document presented here expressly refers again to this DE 10 2020 125 189 A1 . The nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are therefore preferably the magnetic moments of isolated isotopes in the vicinity of the quantum dots NV1, NV2, NV3. Here proximity means that a coupling of the magnetic moments of the relevant isotopes, which form the nuclear quantum dots CI1 ₁ , CI1 ₂ , C11 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 _{1 , CI3 2 ,} CI3 ₃ , with that in the Nearby quantum dot of the nearby quantum bit is possible with the device presented here.

The quantum dots NV1, NV2, NV3 preferably have a magnetic moment of an electron configuration of the respective quantum dot. In the sense of the technical teaching of the document presented here, the quantum dots NV1, NV2, NV3 preferably couple to one another by means of this magnetic moment. One or more quantum dots NV1, NV2, NV3 are preferably paramagnetic centers in the substrate D. Preferably, the Fermi level of the substrate D in the area of a paramagnetic center used as a quantum dot is set so that the paramagnetic center is electrically charged. The electrical charge is preferably negative. In the case of an NV center as a paramagnetic center, the NV center is preferably negatively charged. In the case of an NV center as a paramagnetic center, the NV center is therefore preferably an NV ^- center. The NV centers in the substrate D therefore preferably include NV ^- centers. Doping the substrate D in the area of the paramagnetic center preferably ensures that the paramagnetic center is electrically charged in the intended manner. Isotopes without a magnetic moment as doping atoms preferably dope the material of the substrate D in the area of the relevant quantum dot of the quantum dots NV1, NV2, NV3. These doping atoms preferably shift the Fermi level in the area of this relevant quantum dot without a magnetic moment. These doping atoms therefore preferably shift the Fermi level in the area of the relevant paramagnetic center without a magnetic moment. Preferably, the substrate D essentially comprises, apart from the isotopes, which are used as core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , _{CI3 1 ,} CI3 ₂ , CI3 ₃ of the nuclear quantum bits serve isotopes without nuclear magnetic moment. Since the atoms of III. Main group of the periodic table and the V. Main group of the periodic table generally do not have any stable isotopes without a magnetic moment, so the material of the substrate (D) is preferably mixtures and / or compounds of isotopes without a magnetic moment, for example from isotopes of VI. Main group - e.g. ¹² C, ¹⁴ C, ²⁸ Si, ³⁰ Si, ⁷⁰ Ge, ⁷² Ge, ⁷⁴ Ge, ⁷⁶ Ge, ¹¹² Zn, ¹¹⁴ Zn, ¹¹⁶ Zn, ¹¹⁸ Zn, ¹²⁰ Zn, ¹²² Zn, ¹²⁴ Zn and/or the VI. Main group ¹⁶ E, ¹⁸ E, ³² S, ³⁴ S, ³⁶ S, ⁷⁴ Se, 76 Se, ⁷⁸ Se, ⁸⁰ Se, ⁸² Se, ¹²⁰ Te, ¹²² Te, ¹²⁴ Te, ¹²⁶ Te, ^{128 Te} , ¹³⁰ Te, and /or the II main group ²⁴ Mg ^{, 26} Mg, ⁴⁰ Ca, ⁴² Ca, 44 Ca, 46 Ca, ⁴⁸ Ca, ⁸⁴ Sr, ⁸⁶ Sr, ⁸⁸ Sr, ¹³⁰ Ba, ¹³² Ba ^{, 134} Ba, ¹³⁶ Ba, ¹³⁸ Ba , and/or the II subgroup ⁴⁶ Ti, ⁴⁸ Ti, ⁵⁰ Ti, ⁹⁰ Zr, ⁹⁰ Zr, ⁹² Zr, 94 Zr, ⁹⁶ Zr ^{, 174 Hf, 176 Hf, 178 Hf , and} /or the IV subgroup ⁵⁰ Cr , ⁵² Cr, ⁵³ Cr, ⁹² Mo, ⁹⁴ Mo, ⁹⁶ Mo, ⁹⁸ Mo, ¹⁰⁰ Mo, ¹⁸⁰ W, ¹⁸² W, ¹⁸⁴ W, ¹⁸⁶ W, and/or the VI. Subgroup ⁵⁴ Fe, ⁵⁶ Fe, ⁵⁸ Fe, ⁹⁶ Ru, ⁹⁸ Ru, ¹⁰⁰ Ru, ¹⁰² Ru, ¹⁰⁴ Ru, ¹⁸⁴ 0s, ¹⁸⁶ 0s, ¹⁸⁸ Os, ¹⁹⁰ Os, ¹⁹² Os and/or the VIII subgroup ⁵⁸ Ni, ⁶⁰ Ni, ⁶² Ni, ⁶⁴ Ni, ¹⁰² Pd, ¹⁰² Pd, 104 Pd ^{, 106} Pd, ¹⁰⁸ Pd, ¹¹⁰ Pd, ¹⁹⁰ Pt, ¹⁹² Pt, ¹⁹⁴ Pt, ¹⁹⁶ Pt, ¹⁹⁸ Pt and/or the X subgroup ⁶⁴ Zn, ⁶⁶ Zn, ⁶⁸ Zn, ⁷⁰ Zn, ¹⁰⁶ Cd, 108 Cd, ¹¹⁰ Cd, ¹¹² Cd, ^{114 Cd} , ¹¹⁶ Cd, ¹⁹⁶ Hg, ¹⁹⁸ Hg, ²⁰⁰ Hg, ²⁰² Hg, ²⁰⁴ Hg and/or the lanthanides: ¹³⁶ Ce, ¹³⁸ Ce, ¹⁴⁰ Ce, ¹⁴² Ce ^, 142 Nd, ¹⁴⁴ Nd, ¹⁴⁶ Nd, ¹⁴⁸ Nd, ¹⁵⁰ Nd, 144 Sm, ¹⁴⁶ Sm, ¹⁴⁸ Sm, ¹⁵⁰ Sm, ¹⁵² Sm, ¹⁵⁴ Sm, ¹⁵² Gd, ¹⁵⁴ Gd, ^{156 Gd} , ¹⁵⁸ Gd ^{, 160} Gd, ¹⁵⁶ Dy, ¹⁵⁸ Dy, ¹⁶⁰ Dy, 162 Dy, ¹⁶⁴ Dy, ¹⁶² Er, ¹⁶⁴ Er, ¹⁶⁶ Er, ¹⁶⁸ Er, ¹⁷⁰ Er, ¹⁶⁸ Yb, ¹⁷⁰ Yb, ¹⁷² Yb, ¹⁷⁴ Yb, ¹⁷⁶ Yb, and/or the actinides ²³² Th, ²³⁴ Pa, ²³⁴ U, ²³⁸ U, ²⁴⁴ Pu in question. These isotopes can also be used as doping atoms for doping the substrate (D). If the substrate D comprises diamond and if the quantum dots NV1, NV2, NV3 comprise paramagnetic centers, ³² S, ³⁴ S, ³⁶ S, ¹⁶ O and ¹⁸ O are preferred as doping isotopes for shifting the Fermi level. For the formation of NV centers in diamond as substrate D, an advantageous effect can also be observed for doping with phosphorus, although this is less optimal. The phosphorus isotopes typically have a magnetic moment that interacts with the electron configuration of the paramagnetic centers. However, this interaction is typically undesirable.

Light source LD

According to the proposal, the proposed deployable quantum computer QC preferably comprises a light source LD. The light source LD is preferably a laser which can irradiate quantum dots NV1, NV2, NV3 of the deployable quantum computer with pump radiation LB of a pump radiation wavelength λ _pmp . The light source LD preferably irradiates the relevant quantum dots NV1, NV2, NV3 with pump radiation LB, which is pulse-modulated in its time intensity profile, i.e. preferably pulsed.

Preferably, the light source LD can emit light pulses of the pump radiation LB at light pulse start times t _sp that can be predetermined by the control device µC, based on a reference time t _0p , with a light pulse duration t _dp . A control device µC of the deployable quantum computer preferably controls the light source LD with the aid of a light source driver LDRV via a control data bus SDB. The light source driver LDRV supplies the light source LD with energy. This energy supply to the light source LED typically depends on control commands that the light source driver LDRV receives from the control device µC via the control data bus SDB. The radiation power of the pump radiation LB emitted by the light source LD typically depends on control commands that the light source driver LDRV receives from the control device μC via the control data bus SDB, and on one or more transmission signals S5. The light source LD is preferably a semiconductor laser. Most preferably, the LED light source is a laser diode. The use of an LED (light-emitting diode) as a light source LD is also conceivable. In the exemplary use of NV centers as paramagnetic centers NV1, NV2, NV3 in diamond as quantum dots, the light from the light source LD used as pump radiation LB preferably has a wavelength in a wavelength range of 400 nm to 700 nm wavelength and/or better 450 nm to 650 nm and/or better 500 nm to 550 nm and/or better 515 nm to 540 nm. In the course of developing the technical content of this document, a wavelength of 532 nm of the electromagnetic radiation from the light source LD used as pump radiation LB gave good results. The light source LD preferably comprises a laser, which is preferably a semiconductor laser. In the case of NV centers as paramagnetic centers in diamond as substrate D, a laser diode from Osram of the type PLT5 520B with a 520 nm wavelength has proven itself as an exemplary light source LD for irradiating the NV centers in diamond with pump radiation LB. The deployable quantum computer QC according to the proposal preferably comprises said light source driver LDRV, which controls the emission of the pump radiation LB by the light source LD.

A waveform generator WFG preferably controls the light source driver LDRV and thus the light source LD by means of a transmission signal S5. The waveform generator WFG generates the transmission signal S5 preferably synchronized in time with the radio frequency and microwave signals from the microwave and/or radio wave frequency generator MW/RF-AWFG is generated to generate largely freely definable waveforms (English: arbitrary wave form generator) and radiates mWA into the substrate D using a microwave and/or radio wave antenna. The microwave and/or radio wave antenna mWA thus irradiates the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , C12 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in a fixed time period Phase relationship to the light pulses of the irradiation of the irradiation of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ with pump radiation LB through the light source LD. Typically, the microwave and/or radio wave frequency generator MW/RF-AWFG synchronizes itself to the waveform generator WFG on the transmission signal S5, preferably on the transmission signal S5. This ensures that the phase relationship between the radio and microwave signals from the microwave and/or radio wave frequency generator MW/RF-AWFG on the one hand and the light pulses from the light source LD on the other hand have a predeterminable phase relationship to one another. Preferably, the computer core CPU of the control device µC of the deployable quantum computer QC sets the operating parameters of the waveform generator WFG and the microwave and/or radio wave frequency generator MW/RF-AWFG in accordance with the desired quantum operation in such a way that the quantum states of the quantum dots NV1, NV2, NV3 and the Core quantum states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ can be manipulated as intended.

The light source LD preferably comprises a photodetector. The system preferably includes light source LD and light source driver LDRV and a controller. The photodetector PD of the light source LD can be, for example, a photodiode, which typically monitors the intensity of the pump radiation LB emitted by the light source LD. The controller is preferably part of the light source driver LDRV. The light source driver LDRV preferably drives the light source LD depending on the transmission signal S5. The controller is preferably a P controller or better an I controller or better a PI controller or better a PID controller or a controller with a frequency-optimized frequency response of the gain of the open control loop or the loop gain. The controller preferably compares the value of the measurement signal from the photodetector of the light source LD with the transmission signal S5 from the waveform generator WFG. Depending on the comparison result of the value of the transmission signal S5 with the value of the measurement signal of the photodetector of the light source LD, the controller of the light source LD then regulates the intensity of the pump radiation LB. The controller of the light source LD preferably regulates the intensity of the pump radiation LB by changing the driving power of the light source driver LDRV. As a result, in the ideal case, in the steady state, the intensity of the pump radiation LB essentially corresponds to the value of the transmission signal S5, apart from control deviations. Ideally, the controller of the light source driver LDRV has an analog-to-digital converter and a data interface to the internal control data bus SDB of the deployable quantum computer QC. In this case, the controller and/or a control computer of the light source driver LDRV and/or a control computer of the light source LD can, for example, via the control data bus SDB of the deployable quantum computer QC, which are controlled by the controller of the light source driver LDRV of the light source LD and/or the control computer of the light source LD and / or provide the controller of the light source driver LDRV detected intensity values of the pump radiation LB to the control device µC of the deployable quantum computer QC. In this case, the controller and / or said control computer of the light source LD and / or the control computer of the light source LD can, for example, via the control data bus SDB of the deployable quantum computer QC, the other operating parameters of the light source LD, for example through an analog-to-digital converter and / or sensors within the light source LD and / or the light source driver LDRV, such as respective operating voltages, respective temperatures or the like, also make available to the control device µC of the deployable quantum computer QC. An amplifier of the light source LD and/or an amplifier of the light source driver LDRV preferably amplify the signal of the photodetector of the light source LD before, for example, the analog-to-digital converter of the controller of the light source driver LDRV converts this into a digital measurement signal for the controller of the light source driver LDRV Light source LD converts. The control device µC can, for example, configure the light source LD and/or the light source driver LDRV and their components via the control data bus SDB. Such configuration goals can, for example, but not only, the controller of the light source driver LDRV of the light source LD and its control parameters and / or the gain and / or the frequency response of the amplifier of the light source LD and / or the gain and / or the frequency response of the amplifier of the light source driver LDRV and be their parameters. The light source driver LDRV and the light source LD can form a unit. The light source driver LDRV and the light source LD can have one or more common control computers and/or one or more common analog-to-digital converters. For setting analog control parameters, the light source LD and/or the light source driver LD can have one or more digital-to-analog converters provide analog control levels within the light source LD and/or the light source driver LD. The control device μC of the quantum computer QC preferably controls these digital-to-analog converters via the control data bus SDB. The possibly existing control computer of the light source LD and/or the possibly existing control computer of the LED driver LDRV can also control the digital-to-analog converters.

Optical system

The optical system OS preferably includes a confocal microscope. The light source LD emits the pump radiation LB. In the example of the 1 the pump radiation LB passes through the dichroic mirror DBS. The optical system OS focuses the pump radiation LB on quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , C12 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in the focal point of the optical System OS. The optical system OS prefers to use its confocal microscope. The irradiation of the quantum dots NV1, NV2, NV3 typically causes the quantum dots NV1, NV2, NV3 to emit fluorescent radiation FL. The optical system OS typically detects at least part of the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The optical system OS supplies this detected fluorescence radiation FL to the photodetector PD via the dichroic mirror DBS. The dichroic mirror DBS or another device preferably separates the pump radiation LB and the fluorescent radiation FL from one another in such a way that essentially only fluorescent radiation FL reaches the photodetector PD. Instead of a dichroic mirror DBS, the quantum computer QC proposed here can therefore also include a combination of a semi-transparent mirror and an optical filter. The optical filter is then preferably arranged relative to the semi-transparent mirror on the side of the photodetector PD. The optical filter then preferably allows radiation with the fluorescence wavelength λ _fl of the fluorescence radiation FL to pass through essentially undamped. The optical filter then preferably essentially does not allow radiation with the pump radiation wavelength λ _pmp of the pump radiation LB to pass through. In the example of the 1 the proposed quantum computer QC has another semi-transparent or partially reflecting mirror STM. In the example of the 1 the further semi-transparent or partially reflecting mirror STM splits off part of the fluorescent radiation FL. The further semi-transparent or partially reflecting mirror STM supplies this divided fluorescent radiation FL to an exemplary first camera CM1. The first camera CM1 captures an image of the quantum dots NV1, NV2, NV3 emitting fluorescent radiation FL. In the example, the 1 the control device μC accesses the first camera CM1 and the captured image of the first camera CM1. For example, a user can access the image of the first camera CM1 via the external data bus EXTDB or another interface of the control device µC via the control computer µC and control parts of the quantum computer QC depending on the captured image of the first camera CM1. The computer core CPU of the control device µC can also, for example, query the captured image of the first camera CM1 via the control data bus SDB and then evaluate it or store it in a memory RAM, NVM or process it in some other way. For example, the computer core CPU of the control device µC can execute an image processing program. For example, the computer core CPU of the control device µC or another suitable sub-device of the quantum computer QC can determine a mechanical offset of the quantum dots NV1, NV2, NV3 relative to the optical system OS and determine an offset vector, for example by evaluating the image captured by the first camera CM1. The computer core CPU of the control device µC or the other suitable sub-device of the quantum computer QC preferably corrects this determined offset of the quantum dots NV1, NV2, NV3 relative to the optical system OS. For example, the computer core CPU of the control device µC or the other suitable sub-device of the quantum computer QC can eliminate the determined offset vector by means of a translational positioning device in the X direction XT and/or a translational positioning device in the Y direction YT. For this purpose, the translational positioning device preferably shifts the substrate D with the quantum ALU from quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ in the X direction XT. CI3 ₂ , CI3 ₃ in the x direction in such a way that the X component of the detected offset vector preferably becomes essentially 0. For example, the control device μC can preferably control the translational positioning device XT in the X direction via the control data bus SDB by means of an X control device GDX and query operating parameters of the positioning device XT in the X direction. For this purpose, the X control device GDX for the translational positioning device XT in the X direction and the translational positioning device XT in the X direction is preferably connected to the control data bus SDB. The computer core CPU of the control device μC or the other suitable sub-device of the quantum computer QC preferably carry out a control algorithm that corresponds to a PI or PI controller or another suitable controller. Furthermore, the translational positioning preferably shifts direction in the Y direction YT, the substrate D with the quantum ALU made up of quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in the Y direction in such a way that the Y component of the detected offset vector preferably becomes essentially 0. For example, the control device μC can preferably control the translational positioning device YT in the Y direction via the control data bus SDB by means of a Y control device GDY for the translational positioning device YT in the Y direction and query operating parameters of the positioning device YT in the Y direction. For this purpose, the Y control device GDY for the translational positioning device YT in the Y direction is preferably connected to the control data bus SDB. The computer core CPU of the control device μC or the other suitable sub-device of the quantum computer QC preferably carry out a control algorithm that corresponds to a PI or PI controller or another suitable controller. The quantum computer QC preferably also has a device for refocusing. For example, the optical system OS can comprise a sub-device that enables the optical system OS to be displaced in the Z direction relative to the substrate D. The computer core CPU of the control device µC can preferably control this sub-device to shift the optical system OS in the Z direction via the control data bus STB. Preferably, the computer core CPU of the control device µC can access operating parameters of this sub-device for shifting the optical system OS in the Z direction via the control data bus STB and preferably automatically focus the confocal microscope of the optical system OS. The computer core CPU of the control device µC preferably regulates the distance between the optical system OS and substrate D via the control data bus STB in a manner dependent on the captured image of the first camera CM1 using this sub-device to shift the optical system OS in the Z direction, that the focus of the captured images of the first camera is on the fluorescent quantum dots NV1, NV2, NV3 and remains so in the event of mechanical disturbances. If the control device µC reduces or suppresses the fluorescence radiation FL of such quantum dots NV1, NV2, NV3 too far by manipulating the quantum state of quantum dots NV1, NV2, NV3, the control device µC preferably no longer takes the fluorescence radiation FL of these quantum dots NV1, NV2, NV3 into account the duration of this state of these quantum dots NV1, NV2, NV3 when controlling the position of the substrate D relative to the optical system OS or when controlling the focus of the optical system OS. If the control device µC enables or increases the fluorescence radiation FL of such quantum dots NV1, NV2, NV3 to a sufficient extent by manipulating the quantum state of quantum dots NV1, NV2, NV3, the control device µC preferably takes the fluorescence radiation FL of these quantum dots NV1, NV2, NV3 into account again the duration of this state of these quantum dots NV1, NV2, NV3 when controlling the position of the substrate D relative to the optical system OS or when controlling the focus of the optical system OS. The proposed quantum computer QC therefore preferably comprises one or more control loops for stabilizing the spatial position of the quantum dots NV1, NV2, NV3 and/or nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ relative to the focus point of the optical system OS and possibly preferably one or more control loops for stabilizing the focus of the optical system OS on the quantum dots NV1, NV2, NV3 and/or the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the substrate D.

If necessary, the control device µC readjusts the light source LD and/or the light source driver LDRV depending on the captured image of the first camera CM1. For this purpose, the light source driver LDRV is preferably connected to the control data bus SDB. The computer core CPU can then control the light source driver LDRV via this control data bus STB and preferably query its operating parameters. It is conceivable that the proposed quantum computer QC includes an optical monitoring device within the light source LD and/or within the light source driver LDRV, for example a monitor photodiode with a monitor diode evaluation device associated with this monitor photodiode, which monitors the intensity of the emission of the pump radiation LB of the light source LD and its Parameters recorded. The computer core CPU of the control device µC can then preferably read out these recorded parameters via the control data bus SDB. The control device µC and/or said optical monitoring device of the light source LD and/or the light source driver LDRV and/or another sub-device of the deployable quantum computer QC can then control the intensity of the emission of the pump radiation LB of the light source LD, for example depending on the value of the transmission signal S5 or another parameter specified by you.

The photodetector PD detects the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The photodetector PD converts the detected fluorescence radiation FL into a receiver output signal S0. An amplifier V preferably amplifies and/or filters the receiver output signal S0. The amplifier V preferably amplifies and/or filters the receiver output signal S0 depending on the transmission signal S5. The amplifier preferably comprises V one or more analog-to-digital converters. The computer core CPU of the control device can preferably query values of these analog-to-digital converters via the control data bus SDB. Preferably, an analog-to-digital converter ADCV of the amplifier, in cooperation with an internal amplifier IVV of the amplifier V, converts the receiver output signal S0 into measured values of sample values of the receiver output signal S0. For this purpose, the amplifier V is preferably connected to the control data bus SDB. The computer core CPU of the control device STV can preferably set and/or query operating parameters of the amplifier V via the control data bus SDB. These operating parameters can be, for example, the gain and/or filter parameters of a filtering that the amplifier V carries out.

Microwave control MW/RF-AWFG, mWA

The deployable quantum computer QC according to the proposal preferably comprises one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . For example, such a device MW/RF-AWFG, mWA can be used to generate an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ one or more microwave/radio frequency generators, each preferably having a freely selectable waveform MW/RF-AWFG, and one or more antennas mWA connected to these via one or more waveguides. These antennas mWA then generate said electromagnetic wave _field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . A simple wire can already serve as an antenna mWA if the quantum dots NV1, NV2, NV3 are arranged at a sufficiently small distance from the wire. The said electromagnetic wave field depends on the respective location of the quantum dots NV1, NV2, NV3 and/or on the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ depends on the output signals of the one or more microwave/radio frequency generators, each preferably having a freely selectable waveform MW/RF-AWFG. The control device µC preferably controls the one or more devices MW/RF-AWFG, mWA via the control data bus SDB for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The transmission signal S5 preferably synchronizes the generation of the electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ by the one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . For example, the transmission signal S5 can generate the electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ by the one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ synchronize with the light source driver LDRV and thus with the emission of the pump radiation LB of the light source LD.

Control device µC

The deployable quantum computer QC preferably comprises the already mentioned control device μC with the computer core CPU. The control device μC is preferably a conventional digital computer in Von Neumann or Harvard architecture. The control device µC preferably comprises a computer core CPU and preferably one or more data and program memories RAM NVM. For example, it can be an ARM controller. For example, the computer core CPU can be an ARM Cortex-A78AE for safety-critical applications. The ARM Cortex-A78AE is characterized by including supporting device parts and functions to meet ISO 26262 ASIL Band ASIL D security requirements. The document presented here therefore proposes, in certain cases, to provide a computer core CPU which supports device parts and functions to meet the ISO 26262 ASIL Band ASIL D safety requirements or functionally equivalent standards such as IEC 61508 and/or IEC 62061:2021, EN 61511, EN 50129, EN 62304, US RTCA DO-178B, US RTCA DO-254, EUROCAE ED-12B. The data and program memory RAM NVM or the multiple data and program memories RAM NVM can be designed in whole or in part as a non-volatile memory NVM and/or in whole or in part as a volatile memory RAM. The data and program memory of the control device µC can be read-only in whole or in part and can be read/write in whole or in part. The data and program memory RAM NVM can include, for example, a RAM, an SRAM, a DRAM, a ROM, an EEPROM, a PROM, a flash memory and/or functionally equivalent memories. The control device µC can include a bootstrap device for loading the start program into the data and program memory. The data and program memory RAM NVM of the control device µC can include a BIOS. The data and program memory RAM NVM of the control device µC can comprise a data memory and/or a program memory. The computer core CPU of the control device µC can include a data interface DBIF for communication with other computer systems, in particular a higher-level central control unit ZSE, and with user interfaces. This data interface DBIF can be wired and/or wireless. The document presented here refers to the relevant literature on data networks.

Control tasks of the control device µC

The control device µC of the proposed deployable quantum computer QC preferably also controls the intensity and modulation of the pump radiation LB and intensity modulation of the light source LD by means of its computer core µC. For this purpose, for example, the computer core CPU of the control device μC can control the time course of the intensity of the pump radiation LB emitted by the light source LD. The time course of the intensity of the pump radiation LB from the light source LD is preferably pulse-modulated. The computer core CPU of the control device µC controls the light source LED using the waveform generator WFG via the light source driver LDRV. The computer core CPU of the control device µC preferably controls the intensity I _p and/or the temporal position t _sp of the pulses and/or the temporal duration t _dp of the pulses of the pulsed pump radiation LB of the light source LD. The computer core CPU of the control device µC of the deployable quantum computer QC can thus determine the states of the quantum dots via this intensity I _p of the pulses of the pump radiation LB and via the temporal position t _sp of the pulses of the pump radiation LB and via the temporal duration t _dp of the pulses of the pump radiation LB NV1, NV2, NV3 of the proposed deployable quantum computer affect QC. Therefore, via this intensity I _p of the pulses of the pump radiation LB and via the temporal position t _sp of the pulses of the pump radiation LB and via the temporal duration t _dp of the pulses of the pump radiation LB, the computer core CPU of the control device µC of the deployable quantum computer QC can determine the states of Couple quantum dots NV1, NV2, NV3 of the quantum dots with each other. The device synchronizes these pulses of the pump radiation LB, for example by means of the computer core CPU of the control device µC and/or by means of suitable synchronizations and/or by means of synchronization signals with microwave and/or signals possibly generated by the microwave and/or radio wave frequency generator MW/RF-AWFG Radio signals for controlling the quantum dots NV1, NV2, NV3 and/or nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , C12 ₃ , CI3 _{1 , CI3 2 ,} CI3 ₃ . Such a synchronization signal can be the transmission signal S5. These microwave and/or radio signals generated by the microwave and/or radio wave frequency generator MW/RF-AWFG also influence the quantum dots NV1, NV2, NV3 depending on the state of the quantum dots NV1, NV2, NV3. By influencing the states of the quantum dots NV1, NV2, NV3 of the proposed deployable quantum computer QC, the computer core CPU of the control device µC can typically also influence the states of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and possibly the states of nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ with states of quantum dots NV1, NV2, NV3 couple. Via such influences on the states of the quantum dots NV1, NV2, NV3 of the proposed deployable quantum computer QC, the computer core CPU of the control device µC can typically also influence the states of the nuclear core quantum dots CI1, CI2, CI3 and, if necessary, the states of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ with each other.

Said computer core CPU of the control device µC preferably controls the one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . These one or more devices MW/RF-AWFG, mWA for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , C12 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ preferably generate one or more possibly overlapping electromagnetic fields at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . These electromagnetic fields are preferably designed so that they have a suitable frequency, in particular a microwave and/or radio wave frequency, f _HF , which is typically modulated with a time envelope curve in pulse form. Preferably, the generation of the pulses of these pulsed electromagnetic fields with microwave and/or radio wave frequency f _HF coincides with the generation of the pulses of the pump radiation LB of the light source LED for example, synchronized via the transmission signal S5. Such a pulse of these pulsed electromagnetic fields with microwave and/or radio wave frequency f _HF preferably begins at a pulse start time t _spHF relative to the reference time t _0HF and preferably has a pulse duration t _dHF . The said computer core CPU of the control device µC preferably controls both the one or more devices MW/RF-AWFG for generating the said electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The said computer core CPU of the control device µC preferably sets the frequency of the electromagnetic field f _HF , which the one or more devices MW/RF-AWFG use to generate an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . The said computer core CPU of the control device µC preferably also provides a pulse start time t _spHF relative to the reference time t _0HF and possibly a pulse duration t _dHF of a temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generation of an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in pulse form. In addition, said computer core CPU of the control device µC also preferably sets the amplitude I _pHF of this pulse that these devices MW/RF-AWFG, mWA generate.

In addition, the computer core CPU of the control device µC controls, if necessary, other functions of the deployable quantum computer QC and its sub-devices and methods. The quantum dots NV1, NV2, NV3 and the pairs of two quantum dots and the pairs of one quantum dot and one nuclear core quantum dot typically have different resonance frequencies f _HF . The cause is, firstly, the different spatial distances between the quantum dots within the different pairs of two quantum dots and, secondly, the different spatial distances within the different pairs of one quantum dot and a nuclear core quantum dot assigned to this quantum dot. Preferably, the computer core CPU of the control device µC measures these resonance frequencies f _HF at the start of operation and/or while still in the production facility in a test run or trial operation. To do this, use the means described above. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 . The computer core CPU of the control device µC preferably stores the resonance frequency values determined in this way in a memory NVM of the control device µC as stored resonance frequencies. This memory is preferably a non-volatile memory NVM. This has the advantage that this determination of the resonance frequencies through a scanning process with a typically step-by-step tuning of the frequency f _HF is then necessary less frequently and is not necessary every time the quantum computer QC is restarted. During operation, the computer core CPU of the control device µC uses these resonance frequencies stored in the memory NVM of the control device µC to set the frequency f _HF of the electromagnetic field to be generated so that one or more devices MW/RF-AWFG, mWA are specifically used to generate an electromagnetic field the state of a very specific quantum dot and/or specifically the state of a very specific pair of quantum dots and/or a very specific pair of a quantum dot and a core quantum dot can specifically influence the states of a very specific group of quantum dots. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 .

The computer core CPU of the control device µC can preferably control the light source driver LDRV via the internal data interface MDBIF and the control data bus SDB and read out operating parameters of the light source driver LDRV, such as internal temperatures, internal supply voltages, etc.

The computer core CPU of the control device µC can preferably control the light source LD via the internal data interface MDBIF and the control data bus SDB and read out operating parameters of the light source LD, such as temperature, light emission intensity, etc.

The computer core CPU of the control device µC can preferably control the waveform generator WFG and read out operating parameters of the waveform generator WFG via the internal data interface MDBIF and the control data bus SDB.

The computer core CPU of the control device µC can preferably control the amplifier V via the internal data interface MDBIF and the control data bus SDB and read out operating parameters of the amplifier V, such as gains and / or filter parameters.

The computer core CPU of the control device µC can preferably via the internal data interface MDBIF and the control data bus SDB capture and read out measured values of the receiver output signal S0 of the photodetector PD amplified and filtered by the amplifier V by analog-to-digital converter ADCV of the amplifier V. If possible, the computer core CPU of the control device µC can preferably configure the photodetector PD via the internal data interface MDBIF and, if necessary, read out further operating parameters, such as a bias voltage or a temperature, or set the bias voltage.

The computer core CPU of the control device µC can preferably configure and read out the first camera CM1 via the internal data interface MDBIF and the control data bus SDB and a first camera interface CIF. The first camera CM1 preferably captures an image of the substrate D. The first camera CM1 preferably captures an image of the distribution of the fluorescence radiation FL of the substrate D and preferably transmits this image to the computer core CPU of the control device μC. The first camera CM1 preferably captures an image of the distribution of the fluorescence radiation FL of the quantum dots NV1, NV2, NV3 of the substrate D and preferably transmits this image to the computer core CPU of the control device µC. The computer core CPU of the control device µC can thus control the first camera CM1 and read out operating parameters and data from the camera CM1.

The computer core CPU of the control device µC can preferably control the X control device GDX for the translational positioning device XT in the

The computer core CPU of the control device µC can preferably control the Y control device GDY for the translational positioning device YT in the Y direction via the internal data interface MDBIF and the control data bus SDB and read out and, if necessary, adapt operating parameters of the Y control device GDY.

The computer core CPU of the control device µC can preferably control the translational positioning device XT in the X direction via the internal data interface MDBIF and the control data bus SDB and via the

The computer core CPU of the control device µC can preferably control the translational positioning device YT in the Y direction via the internal data interface MDBIF and the control data bus SDB and via the Y control device GDY and read out and, if necessary, adapt operating parameters of the translational positioning device YT in the Y direction.

The computer core CPU of the control device µC preferably detects the position of the substrate D relative to the optical system OS. The computer core CPU of the control device µC can, for example and preferably via the internal data interface MDBIF and the control data bus SDB and via the first camera interface CIF and the first camera CIM1 preferably detect this position of the substrate D relative to the optical system OS and changes in this position of the substrate D relative to the optical system OS by means of the Y control device GDY and the translational positioning device YT in the Y direction and by means of the X control device GDX and the translational positioning device XT in the optical system OS.

The computer core CPU of the control device µC can preferably read out and, if necessary, configure a temperature sensor ST via the internal data interface MDBIF and the control data bus SDB.

The computer core CPU of the control device µC can preferably reconfigure or operate differently one or more device parts of the deployable quantum computer QC via the internal data interface MDBIF and the control data bus SDB depending on the temperature detected with the temperature sensor ST. In particular, the computer core CPU of the control device µC can put one or more fans of the quantum computer QC or functionally equivalent cooling devices such as water or oil coolers with corresponding coolant circuits into operation or change their operating parameters so that the temperature detected by the temperature sensor TS remains in a predetermined temperature range. The proposed quantum computer QC can have one or more temperature sensors TS and one or more coolant circuits and/or one or more fans. All suitable fluids can be used as coolants. Air, water and oil are particularly preferred. The cooling typically serves to dissipate waste heat from device parts of the quantum computer QC. Typically, a target temperature in the range of 0°C to 50°C is preferred. A military temperature range of -40°C to 125°C seems sensible for military applications. Instead of a cooling device, the quantum computer QC can also have a heater for air conditioning purposes, whereby the computer core CPU of the control device µC can preferably use the internal data interface set MDBIF and the control data bus SDB, depending on the temperature detected with the temperature sensor ST, then controls this heater so that the interior of the quantum computer QC exceeds a minimum temperature. The heating can be, for example, electrical, chemical or thermonuclear.

The computer core CPU of the control device µC preferably detects the position of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D. The computer core CPU of the control device µC can, for example and preferably, via the internal data interface MDBIF and the control data bus SDB and via the second camera interface CIF2 and the second camera CIM2 preferably capture this position of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D, for example in the side view.

The computer core CPU of the control device µC can preferably configure and read out the second camera CM2 via the internal data interface MDBIF and the control data bus SDB and the second camera interface CIF2. The second camera CM2 preferably captures an image of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D, for example in the side view. For this purpose, a lamp LM with a lamp preferably illuminates the area that the second camera CM2 is intended to capture. The second camera CM2 preferably captures this image and preferably transmits this image to the computer core CPU of the control device μC. The computer core CPU of the control device µC can thus control the second camera CM2 and read out operating parameters and data of the second camera CM2. This second camera CM2 makes it possible to remotely observe and check the positioning process and the positioning of the substrate D relative to the optical system OS by means of the translational positioning device XT in the X direction and the translational positioning device YT in the Y direction and, if necessary, the positioning process and to observe and check the positioning of the substrate D relative to a permanent magnet PM by means of the positioning device PV of this permanent magnet PM, without having to check the housing of the quantum computer QC. The second camera CM2 preferably transmits the image of the observed image area via the second camera interface CIF2, the control data bus SDB, the internal data interface MDBIF, the internal data bus INTDB of the control device µC, the computer core CPU of the control device µC, the external data interface DBIF of the control device µC and the external data bus EXTDB to a higher-level control unit ZSE or another computer that has a suitable human-machine interface. This human-machine interface can have a screen and a keyboard or the like, so that an operator of the quantum computer QC can make inputs here for controlling device parts of the quantum computer QC or the quantum computer QC as a whole. This or another human-machine interface can serve to display calculation results of the quantum computer QC and/or represent status messages of the quantum computer QC, in particular of the computer core CPU of the control device µC and/or operating parameters and/or status messages of device parts of the quantum computer QC. In particular, the human-machine interface can display images and/or video sequences of the first camera CM1 and/or the second camera CM2. These images and/or video sequences can be previously processed for display by the computer core CPU of the control device µC of the quantum computer QC or a computer that is connected to the deployable quantum computer QC via the external data bus EXTDB. The computer can be a central control unit ZSE. For example, it can be false-color images, image sections and distorted images and videos or the like.

The first camera CM1 and/or the second camera CM2 do not necessarily need to be RGB cameras. Rather, they can also be sensitive to radiation that is not visible to humans. The first camera CM1 and/or the second camera CM2 can also be multispectral cameras in order, for example, to be able to optimally observe the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The first camera CM1 preferably includes imaging optics and an imaging photodetector circuit, for example a CCD sensor IC, and camera evaluation electronics that are coupled to the first camera interface CIF. The second camera CM2 preferably comprises a second imaging optics and a second imaging photodetector circuit, for example a second CCD sensor IC, and a second camera evaluation electronics which is coupled to the second camera interface CIF2.

The computer core CPU of the control device µC can preferably control a control device PVC for a positioning device PV of the permanent magnet PM via the internal data interface MDBIF and the control data bus SDB and read out and, if necessary, modify operating parameters of the control device PVC for a positioning device PV of the permanent magnet PM.

For example, the computer core CPU of the control device µC can preferably detect changes in the position of the substrate D relative to the optical system OS and the position of a permanent magnet PM relative to the substrate D, for example in the side view, via the internal data interface MDBIF and the control data bus SDB, and such changes in the position of the Rebalance the permanent magnet PM relative to the substrate D using a positioning device PV of the permanent magnet PV. For this purpose, the computer core CPU of the control device µC preferably uses the control device PVC for a positioning device PV of the permanent magnet PM. The computer core CPU of the control device µC can thereby preferably control the positioning device PV of the permanent magnet PM via the internal data interface MDBIF and the control data bus SDB by means of which the control device PVC and read out and, if necessary, modify operating parameters of the positioning device PV. In particular, the computer core CPU of the control device μC can, for example, preferably control and change the position of the permanent magnet PM via the internal data interface MDBIF and the control data bus SDB by means of the positioning device PV. Preferably, the computer core CPU of the control device µC can detect changes in the position of the permanent magnet PM relative to the substrate D using the second camera CM2 and compensate for them again using the positioning device PV.

The proposed quantum computer QC thus comprises first means (CM1, CM2) for detecting changes in the arrangement of device parts (OS, D, PM) relative to one another, and second means (XT, YT, PV) for undoing the detected changes. The first means can also include functionally equivalent sensors, in particular position sensors. The second means can also include other functionally equivalent actuators.

The computer core CPU of the control device µC can, for example, preferably control a microwave and/or radio wave frequency generator MW/RF-AWFG via the internal data interface MDBIF and the control data bus SDB to generate largely freely definable waveforms (English: arbitrary wave form generator) and its Read operating parameters and adjust if necessary. In particular, for example, the computer core CPU of the control device µC can preferably program or set the generated waveforms of the microwave and / or radio wave frequency generator MW / RF-AWFG via the internal data interface MDBIF and the control data bus SDB or read out the set waveform.

The computer core CPU of the control device µC can, for example, preferably set and configure the microwave and/or radio wave antenna mWA via the internal data interface MDBIF and the control data bus SDB and/or read out such a configuration of the microwave and/or radio wave antenna mWA. The microwave and/or radio wave frequency generator MW/RF-AWFG typically controls the microwave and/or radio wave antenna mWA with the waveforms of the microwave and/or radio wave frequency generator MW/RF-AWFG generated by the microwave and/or radio wave frequency generator MW/RF-AWFG at. The microwave and/or radio wave antenna mWA irradiates the substrate D with the quantum dots NV1, NV2, NV3 with the electromagnetic radiation corresponding to the waveforms of the microwave and/or radio wave frequency generator MW/RF generated by the microwave and/or radio wave frequency generator MW/RF-AWFG -AWFG.

As a result, the electromagnetic radiation manipulates the quantum state of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ in accordance with the waveforms of the microwave and/or radio wave frequency generator MW/RF-AWFG generated by the microwave and/or radio wave frequency generator MW/RF-AWFG , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 _{1 , CI3 2 ,} CI3 ₃ in the substrate D. This allows the computer core CPU of the control device µC to determine the quantum state of the quantum dots NV1, NV2, for example via the internal data interface MDBIF and the control data bus SDB , NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in substrate D. The computer core CPU of the control device µC can typically determine the quantum state of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 via the internal data interface MDBIF and the control data bus SDB by means of the waveform generator WFG and the light source driver LDRV and the light source LD ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in substrate D.

The computer core CPU of the control device µC can, for example, preferably via the internal data interface MDBIF and the control data bus SDB a cooling device KV of the substrate D and possibly in the 1 Control auxiliary devices, not shown, of the cooling device KV of the substrate D and record and read out their status information. The auxiliary device of the cooling device KV of the substrate D can, for example, be a so-called closed loop helium gas cooling system HeCLCS that uses helium as a coolant. The computer core CPU of the control device µC can, for example, preferably control the closed loop helium gas cooling system HeCLCS via the internal data interface MDBIF and the control data bus SDB. For example, this coolant can flow through a cooling surface as a cooling device KV, with the substrate D being attached in a thermally conductive manner on the surface of the cooling surface serving as a cooling device KV and thereby the substrate is cooled by the closed loop helium gas cooling system HeCLCS. Preferably, the translational positioning device XT in the X direction and the translational positioning device YT in the Y direction position the composite of the cooling device KV and substrate D.

The computer core CPU of the control device µC can, for example, preferably control a charging device LDV via the internal data interface MDBIF and the control data bus SDB and read out operating parameters and data from the charging device LDV. Such an operating parameter can be, for example, the voltage value of the mains voltage of the electrical supply network that supplies the charging device LDV with electrical energy.

The computer core CPU of the control device µC can, for example, preferably control a separating device TS via the internal data interface MDBIF and the control data bus SDB and read out operating parameters and data from the separating device TS. For example, the computer core CPU of the control device µC can separate the outputs of the charging device LDV from the first energy reserve BENG and / or the second energy reserve BENG2, so that firstly it no longer charges the first energy reserve BENG and / or the second energy reserve BENG2 with electrical energy and secondly Secondly, the remaining device parts of the quantum computer are not disturbed or are only disturbed to a much lesser extent. For example, the computer core CPU of the control device µC can connect the outputs of the charging device LDV to the first energy reserve BENG and/or to the second energy reserve BENG2, so that it charges the first energy reserve BENG and/or the second energy reserve BENG2 with electrical energy.

The computer core CPU of the control device µC can, for example, preferably control the first energy reserve BENG and/or read out operating parameters and data from the first energy reserve BENG via the internal data interface MDBIF and the control data bus SDB. For example, the first energy reserve BENG can include several submodules that the computer core CPU of the control device µC monitors. For example, the computer core CPU of the control device µC can detect the temperature of these sub-modules and/or the pressure in these sub-modules and/or the state of charge of these sub-modules. For this purpose, the first energy reserve BENG preferably comprises suitable sensors, the values of which the computer core CPU of the control device µC can detect. In the event of an error, the computer core CPU of the control device µC can detect this error in the recorded parameters of these sub-modules and switch faulty sub-modules out of the group and bridge the resulting gap. For this purpose, the first energy reserve BENG preferably comprises suitable switches and/or changeover switches, the switching state of which can be influenced by the computer core CPU of the control device μC.

In this way, the computer core CPU of the control device μC can preferably influence the energy supply of a first energy processing device SRG.

The computer core CPU of the control device µC can, for example, preferably control the first energy processing device SRG via the internal data interface MDBIF and the control data bus SDB and / or record and read out operating parameters and data of the first energy processing device SRG. Typically, the computer core CPU of the control device μC can monitor and control the energy supply to the remaining device parts of the quantum computer QC.

If DMA accesses of the remaining device parts of the quantum computer QC are permitted, these can, for example, preferably via the internal data interface MDBIF and the control data bus SDB by means of a DMA access to the control device µC and/or the memory RAM, NVM of the control device µC and/or the the computer core CPU and/or the control device µC and the data interface DBIF and the external data bus EXTDB access devices outside the quantum computer QC.

The possibly existing internal control computers of device parts of the quantum computer QC can, for example, preferably communicate with devices outside the quantum computer QC via the control device μC and the data interface DBIF and the external data bus EXTDB and exchange data with these external devices. Such external devices can be, for example, control devices of a motor vehicle or the like. In particular, data exchange with the Internet or a comparable data network with a large number of computer systems is conceivable. These computer systems can include, for example, a deployable central control unit ZSE of a deployable quantum computer system QUSYS, part of which can be the deployable quantum computer QC.

The computer core CPU of the control device µC can use the volatile memory RAM of the control Write and read data to the µC device. Typically, the data content of the volatile memory RAM includes program data and/or operating data and/or program instructions.

The computer core CPU of the control device µC can read the data of the non-volatile memory NVM of the control device µC. The non-volatile memory NVM of the control device µC preferably comprises a writable non-volatile memory such as a flash memory. Typically, the data content of the non-volatile memory NVM includes program data and/or operational data and/or program instructions. The data content of a non-volatile and writable memory NVM preferably includes the parameters of the resonance frequencies for driving the core quantum bits CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , C12 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

The computer core CPU of the control device µC can, for example, read the memory RAM, NVM of the control device µC and/or write data to it.

The computer core CPU of the control device µC can preferably access a higher-level computer system, for example a central control unit ZSE and/or the control devices of other quantum computers QC1 to QC16, via the data interface DBIF and the external data bus EXTDB.

The computer core CPU of the control device µC can access the control data bus SDB via the internal data interface MDBIF and other device parts of the deployable quantum computer QC via this control data bus SDB.

The computer core CPU of the control device µC can, for example, preferably control the light source driver LDRV and/or read out operating parameters and data of the light source driver LDRV via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, the light intensity and other adjustable operating parameters. The data that the computer core CPU of the control device µC can read out from the light source driver LDRV via the internal data interface MDBIF and the control data bus SDB can include, for example, current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, this allows the computer core CPU of the control device µC to monitor and control the light source driver LDRV of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the waveform generator WFG and/or read out operating parameters and data from the waveform generator WFG via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, the data of the waveform to be generated of the transmission signal S5 of the waveform generator WFG and/or the speed/frequency of the generation of the thus specified waveform of the generated transmission signal S5 of the waveform generator WFG and other adjustable operating parameters of the waveform generator WFG. The data that the computer core CPU of the control device µC can read out from the waveform generator WFG via the internal data interface MDBIF and the control data bus SDB can include, for example, current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, the computer core CPU of the control device μC can monitor and control the waveform generator WFG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the amplifier V and / or read out operating parameters and data of the amplifier V via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, the gain and/or filter parameters of the amplifier V and other adjustable operating parameters of the amplifier V. The data that the computer core CPU of the control device µC can read from the amplifier V via the internal data interface MDBIF and the control data bus SDB can include, for example, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, the computer core CPU of the control device µC can monitor and control the amplifier V of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the photodetector PD and/or read out operating parameters and data from the photodetector PD via the internal data interface MDBIF and the control data bus SDB. The control data can be, for example, the gain and/or filter parameters of a control circuit that may be present and integrated into the photodetector PD, which controls the actual photon-sensitive element of the photodetector PD and detects the values relevant for the detection of photons and converts them into a readable signal. The data that the computer core CPU of the control device µC can read from the photodetector PD via the internal data interface MDBIF and the control data bus SDB can, for example, be internal Current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom. Typically, the computer core CPU of the control device µC can monitor and control the photodetector PD of the quantum computer QC. In the simplest case, it can also be a completely passive photodetector PD without any intelligence, which only transmits an analog output signal to the amplifier V.

The computer core CPU of the control device µC can, for example, preferably control the first camera CM1 and/or read out operating parameters and data of the first camera CM1 via the internal data interface MDBIF and the control data bus SDB and a first camera interface CIF. The control data can include, for example, operating parameters of the first camera CM1 such as brightness, contrast, color settings, aperture, focus, etc. of the first camera CM1 and other adjustable operating parameters of the first camera CM1. The data that the computer core CPU of the control device µC can read out from the first camera CM1 via the internal data interface MDBIF and the control data bus SDB can, for example, be the image data, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and from there include derived values. Typically, the computer core CPU of the control device µC can monitor and control the first camera CM1 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the first camera interface CIF and/or read out operating parameters and data from the first camera interface CIF via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the first camera interface CIF such as memory depth, DMA access parameters and other adjustable operating parameters of the first camera interface CIF. The data that the computer core CPU of the control device µC can read out from the first camera interface CIF via the internal data interface MDBIF and the control data bus SDB can, for example, be the image data of the first camera CM1, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived from them. Typically, the computer core CPU of the control device µC can thereby monitor and control the first camera interface CIF of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second camera CM2 and/or read out operating parameters and data of the second camera CM2 via the internal data interface MDBIF and the control data bus SDB and a second camera interface CIF2. The control data can include, for example, operating parameters of the second camera CM2 such as brightness, contrast, color settings, aperture, focus, etc. of the second camera CM2 and other adjustable operating parameters of the second camera CM2. The data that the computer core CPU of the control device µC can read out from the second camera CM2 via the internal data interface MDBIF and the control data bus SDB can include, for example, the image data, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and from there include derived values. Typically, the computer core CPU of the control device µC can monitor and control the second camera CM2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second camera interface CIF2 and/or read out operating parameters and data from the second first camera interface CIF2 via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second camera interface CIF2 such as memory depth, DMA access parameters and other adjustable operating parameters of the second first camera interface CIF2. The data that the computer core CPU of the control device µC can read out from the second camera interface CIF2 via the internal data interface MDBIF and the control data bus SDB can, for example, be the image data of the second camera CM2, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived from them. Typically, the computer core CPU of the control device µC can monitor and control the second camera interface CIF2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control a lamp with a lamp LM for illuminating the field of view of the second camera CM2 via the internal data interface MDBIF and the control data bus SDB and / or read out operating parameters and data of the lamp with the lamp LM. The control data can include, for example, operating parameters of the lamp with the lamp LM such as brightness, orientation and other adjustable operating parameters of the lamp with the lamp LM. The data that the computer core CPU of the control device µC can read out from the lamp with the lamp LM via the internal data interface MDBIF and the control data bus SDB, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom. Typically, the computer core CPU of the control device µC can monitor and control the lamp with the lamp LM of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control one or more temperature sensors ST and/or read out operating parameters and data of the one or more temperature sensors ST via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the one or more temperature sensors ST and other adjustable operating parameters of the one or more temperature sensors ST. The data that the computer core CPU of the control device µC can read out from the one or more temperature sensors ST via the internal data interface MDBIF and the control data bus SDB can include temperature data, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and include values derived from it. Typically, this allows the computer core CPU of the control device µC to monitor and control the one or more temperature sensors ST of the quantum computer QC and the quantum computer QC itself.

The one temperature sensor ST or the multiple temperature sensors ST can include, for example, NTC resistors, PTC resistors, PN junctions, thermocouples (e.g. platinum/rhodium thermocouples) or the like and/or evaluation electronics as temperature-sensitive sensor elements.

If the quantum computer QC is to be used in hot or very cold environments, the quantum computer QC can have one or more heating devices and/or cooling devices for the quantum computer QC as a whole. If the quantum computer QC is to be used in hot or very cold environments, the computer core CPU of the control device µC can then, for example, preferably via the internal data interface MDBIF and the control data bus SDB these one or more heating devices for the quantum computer QC and / or these one or more cooling devices for the quantum computer QC as a whole and / or read out operating parameters and data of these one or more heating devices and / or cooling devices for the quantum computer QC. The control data may include, for example, operating parameters of the one or more heating devices and/or one or more cooling devices for the quantum computer QC and other adjustable operating parameters of the one or more heating devices and/or cooling devices for the quantum computer QC. The data that the computer core CPU of the control device µC can read out from the one or more heating devices and / or cooling devices for the quantum computer QC via the internal data interface MDBIF and the control data bus SDB can be temperature data, internal current strengths, internal values, electrical voltages, operating temperatures, Include identification data such as the serial number etc. and values derived therefrom. Typically, this allows the computer core CPU of the control device µC to monitor and control the one or more heating devices and/or cooling devices for the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the microwave and/or radio wave frequency generator MW/RF-AWFG via the internal data interface MDBIF and the control data bus SDB to generate largely freely definable waveforms and/or operating parameters and data of the microwave and/or radio wave frequency generator Read out MW/RF-AWFG. The control data can, for example, be operating parameters of the microwave and/or radio wave frequency generator MW/RF-AWFG, such as waveform, wave frequency, amplitude and time delay compared to a synchronization signal, such as the transmission signal S5, and other adjustable operating parameters of the microwave and/or radio wave frequency generator MW/RF -AWFG include. The data that the computer core CPU of the control device µC can read out from the microwave and/or radio wave frequency generator MW/RF-AWFG via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived from them etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the magnetic field sensors MSx, MSy, MSz and/or operating parameters and/or operating parameters via the internal data interface MDBIF and the control data bus SDB and via the magnetic field controllers MFSx, MFSy, MFSz Read out data from the magnetic field sensors MSx, MSy, MSz. The control data can include, for example, operating parameters of the magnetic field sensors MSx, MSy, MSz such as sensitivity, current supply and other adjustable operating parameters of the microwave and/or radio wave frequency generator MW/RF-AWFG. The data that the computer core CPU of the control device µC can read out from the magnetic field sensors MSx, MSy, MSz via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurements, internal current strengths, internal values of electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived from it etc. include. Typically, the computer core CPU of the control device µC can monitor and control the magnetic field sensors MSx, MSy, MSz of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the first magnetic field controller MFSx and/or read out operating parameters and data of the first magnetic field controller MFSx via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the first magnetic field control MFSx such as the strength of the magnetic flux density B _x to be set in the direction of the first direction, the current supply to be set to the first magnetic field generating means MGx and other adjustable operating parameters of the first magnetic field control MFSx. The data that the computer core CPU of the control device µC can read out from the first magnetic field controller MFSx via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurement values, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and those derived therefrom Values etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the first magnetic field control MFSx of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second magnetic field control MFSy and/or read out operating parameters and data of the second magnetic field control MFSy via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second magnetic field control MFSy, such as the strength of the magnetic flux density B _y to be set in the direction of the second direction, the current supply to be set to the second magnetic field generating means MGy and other adjustable operating parameters of the second magnetic field control MFSy. The data that the computer core CPU of the control device µC can read out from the second magnetic field controller MFSy via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurements, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and those derived therefrom Values etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the second magnetic field control MFSy of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the third magnetic field controller MFSz and/or read out operating parameters and data from the third magnetic field controller MFSz via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the third magnetic field control MFSz such as the strength of the magnetic flux density B _z to be set in the direction of the third direction, the current supply to be set to the third magnetic field generating means MGy and other adjustable operating parameters of the third magnetic field control MFSz. The data that the computer core CPU of the control device µC can read out from the third magnetic field controller MFSz via the internal data interface MDBIF and the control data bus SDB can include the magnetic field measurement values, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and those derived therefrom Values etc. include. Typically, the computer core CPU of the control device µC can thereby monitor and control the third magnetic field control MFSz of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the first energy processing device SRG and/or read out operating parameters and data of the first energy processing device SRG via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the first energy processing device SRG, such as the voltage values to be delivered to other device parts and maximum current intensities and other adjustable operating parameters of the first energy processing device SRG. The data that the computer core CPU of the control device µC can read out from the first energy processing device SRG via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom, etc. include. Typically, the computer core CPU of the control device µC can do this Monitor and control the first energy processing device SRG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the second energy processing device SRG2 and/or read out operating parameters and data of the second energy processing device SRG2 via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second energy processing device SRG2, such as the voltage values to be delivered to other device parts and maximum current intensities and other adjustable operating parameters of the second energy processing device SRG2. The data that the computer core CPU of the control device µC can read out from the second energy processing device SRG2 via the internal data interface MDBIF and the control data bus SDB can include internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom, etc. include. Typically, the computer core CPU of the control device μC can thereby monitor and control the second energy processing device SRG2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the energy reserve BENG and/or read out operating parameters and data from the energy reserve BENG via the internal data interface MDBIF and the control data bus SDB. If the energy reserve BENG has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the energy reserve BENG via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the energy reserve BENG such as maximum temperatures, etc. The control and monitoring device of the BENG energy reserve preferably has means for monitoring important, in particular safety-relevant, operating parameters of the BENG energy reserve. These means can include temperature sensors, voltage and current sensors or pressure sensors for measuring the internal pressure of battery cells. The data that the computer core CPU of the control device µC can read out from the energy reserve BENG via the internal data interface MDBIF and the control data bus SDB can, for example, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom etc. include. Typically, the computer core CPU of the control device µC can monitor and control the energy reserve BENG of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the energy reserve BENG and/or read out operating parameters and data from the second energy reserve BENG2 via the internal data interface MDBIF and the control data bus SDB. If the second energy reserve BENG2 has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the second energy reserve BENG2 via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the second energy reserve BENG2 such as maximum temperatures, etc. The control and monitoring device of the second energy reserve BENG2 preferably has means for monitoring important, in particular safety-relevant, operating parameters of the second energy reserve BENG2. These means can include temperature sensors, voltage and current sensors or pressure sensors for measuring the internal pressure of battery cells. The data that the computer core CPU of the control device µC can read out from the second energy reserve BENG2 via the internal data interface MDBIF and the control data bus SDB can, for example, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number, etc. and values derived therefrom, etc . include. Typically, this allows the computer core CPU of the control device µC to monitor and control the second energy reserve BENG2 of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the separating device TS and/or read out operating parameters and data of the separating device TS via the internal data interface MDBIF and the control data bus SDB. If the separating device TS has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the separating device TS via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the separating device TS such as closing status (connected/disconnected), maximum temperatures, etc. The control and monitoring device of the separating device TS preferably has means for monitoring important, in particular safety-relevant, operating parameters of the separating device TS. These funds can include temperature sensors, voltage and current sensors. The data that the computer core CPU of the control device µC can read out from the separating device TS via the internal data interface MDBIF and the control data bus SDB can, for example, internal current strengths, internal values, electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom etc. include. Typically, the computer core CPU of the control device µC can monitor and control the separation device TS of the quantum computer QC.

The computer core CPU of the control device µC can, for example, preferably control the charging device LDV and/or read out operating parameters and data from the charging device LDV via the internal data interface MDBIF and the control data bus SDB. If the charging device LDV has its own control and monitoring device, the computer core CPU of the control device µC can, for example, preferably send control data to this control and monitoring device of the charging device LDV via the internal data interface MDBIF and the control data bus SDB. The control data can include, for example, operating parameters of the charging device LDV such as mains voltage of the power supply PWR of the charging device LDV, output voltages of the charging device LDV to be set, maximum temperatures, etc. The control and monitoring device of the separating device TS preferably has means for monitoring important, in particular safety-relevant, operating parameters of the loading device LDV.

These means may include temperature sensors, voltage and current sensors. The data that the computer core CPU of the control device µC can read out from the charging device LDV via the internal data interface MDBIF and the control data bus SDB can, for example, be the actual mains voltage of the power supply PWR of the charging device LDV, actually set output voltages of the charging device LDV, internal current strengths, internal Values include electrical voltages, operating temperatures, identification data such as the serial number etc. and values derived therefrom etc. Typically, the computer core CPU of the control device µC can monitor and control the charging device LDV of the quantum computer QC.

• - einen oder mehrere Werte von Betriebsspannungen von Vorrichtungsteilen des Quantencomputers QC,
• - einen oder mehrere Werte von Stromaufnahmen von Vorrichtungsteilen des Quantencomputers QC,
• - den Prozessortakt des Rechnerkerns CPU der Steuervorrichtung µC des Quantencomputers QC und/oder dessen Frequenz,
• - die Prozessortakte anderer Vorrichtungsteile des Quantencomputers QC und/oder deren Frequenz,
• - die Lichtabgabe der Lichtquelle LD des Quantencomputers QC, insbesondere die Intensität der Pumpstrahlung LB der Lichtquelle LD,
• - die Signalerzeugung des der Wellenformgenerators WFG des Quantencomputers QC,
• - die Funktionstüchtigkeit der Datenschnittstelle DBIF,
• - die Funktionstüchtigkeit der die internen Datenschnittstelle MDBIF,
• - die Funktionstüchtigkeit des Lichtquellentreibers LDRV,
• - die Funktionstüchtigkeit des Verstärkers V,
• - die Funktionstüchtigkeit der Fotodetektor PD,
• - die Temperatur mittels eines Temperatursensors ST,
• - die Funktionstüchtigkeit des Mikrowellen- und/oder Radiowellenfrequenzgenerators MW/RF-AWFG zur Erzeugung weitestgehend frei vorgebbarer Wellenformen,
• - die Funktionstüchtigkeit der Magnetfeldsensoren MSx, MSy, MSz,
• - die Funktionstüchtigkeit der Magnetfeldsteuerungen MFSx, MFSy, MFSz,
• - die Funktionstüchtigkeit der ersten Energieaufbereitungsvorrichtung SRG,
• - die Funktionstüchtigkeit der zweiten Energieaufbereitungsvorrichtung SRG2,
• - die Funktionstüchtigkeit der Energiereserve BENG,
• - die Funktionstüchtigkeit der zweiten Energiereserve BENG2,
• - die Funktionstüchtigkeit der Trennvorrichtung TS,
• - die Funktionstüchtigkeit der Ladevorrichtung LDV.
• - -die Detektionsfähigkeit von elektromagnetischer Strahlung eines Fotodetektors
• - -die bestimmungsgemäß korrekte Erzeugung elektromagnetischer Felder, insbesondere von Mikrowellenfeldern und/oder Radiowellenfeldern eine Vorrichtung des Quantencomputers QC zur Manipulation eines oder mehrerer Quantenbits QUB,
• - -den komplexen und/oder realen und/oder imaginären Leitwert einer Leitung und der Mikrowellen- und/oder Radiowellenantenne MWA, die Teil der Vorrichtung des Quantencomputers QC zur Manipulation eines oder mehrerer Quantenpunkte NV1, NV2, NV3 ist.

The deployable quantum computer QC according to the proposal preferably has a quantum computer monitoring device QUV, which monitors the quantum computer QC while the quantum computer QC executes a quantum computer program with a quantum computer program sequence, which is preferably stored in its memory RAM, NVM. The document presented here refers to the as yet unpublished German patent application DE 10 2021 110 964.7 and any subsequent registrations resulting from priority claims. This quantum computer monitoring device QUV monitors the correct quantum computer program flow of the quantum computer program of the quantum computer QC. The quantum computer monitoring device QUV preferably monitors at least the value and/or value progression of at least one, better several and optimally all of the following operating parameters:

• - one or more values of operating voltages of device parts of the quantum computer QC,
• - one or more values of current consumption of device parts of the quantum computer QC,
• - the processor clock of the computer core CPU of the control device µC of the quantum computer QC and / or its frequency,
• - the processor clocks of other device parts of the quantum computer QC and/or their frequency,
• - the light output of the light source LD of the quantum computer QC, in particular the intensity of the pump radiation LB of the light source LD,
• - the signal generation of the waveform generator WFG of the quantum computer QC,
• - the functionality of the DBIF data interface,
• - the functionality of the internal data interface MDBIF,
• - the functionality of the light source driver LDRV,
• - the functionality of the amplifier V,
• - the functionality of the photodetector PD,
• - the temperature using a temperature sensor ST,
• - the functionality of the microwave and/or radio wave frequency generator MW/RF-AWFG to generate largely freely definable waveforms,
• - the functionality of the magnetic field sensors MSx, MSy, MSz,
• - the functionality of the magnetic field controls MFSx, MFSy, MFSz,
• - the functionality of the first energy processing device SRG,
• - the functionality of the second energy processing device SRG2,
• - the functionality of the BENG energy reserve,
• - the functionality of the second energy reserve BENG2,
• - the functionality of the separating device TS,
• - the functionality of the LDV charging device.
• - -the detection capability of electromagnetic radiation of a photodetector
• - - the correct generation of electromagnetic fields, in particular microwave fields and / or radio wave fields, a device of the quantum computer QC for manipulating one or more quantum bits QUB,
• - -the complex and/or real and/or imaginary conductance of a line and the microwave and/or radio wave antenna MWA, which is part of the device of the quantum computer QC for manipulating one or more quantum dots NV1, NV2, NV3.

Quantum computer monitoring device QUV

Typically, the T2 times of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 _{1 , CI3 2 ,} CI3 ₃ are limited. Therefore, there are time breaks between two quantum computer calculations, during which a quantum computer monitoring device QUV of the quantum computer QC can check the functionality of the remaining quantum computer QC.

Typically, the quantum computer QC carries out its quantum computer calculations within initial periods of time, which are typically shorter than the T2 times of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are, through. The quantum computer monitoring device QUV preferably carries out tests on the remaining device parts of the quantum computer QC within second time periods. The first periods are preferably different from the second periods. A quantum computer calculation in the sense of this document includes at least one quantum operation, such as, for example, an initialization of one or more quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or, for example, the execution of a quantum gate such as a CNOT operation or a CCNOT operation or a Hadamard gate or a π pulse or an X gate etc.

In this context, the document presented here refers to the book by Steven Prawer (editor), Igor Aharonovich (editor), “Quantum Information Processing with Diamond: Principles and Applications”, Woodhead Publishing Series in Electronic and Optical Materials, Volume 63, Woodhead Publishing , May 8, 2014, ISBN-10: 0857096567, ISBN-13: 978-0857096562.

Since the result of a quantum calculation of the quantum computer QC only provides correct results with a certain statistic, the quantum computer monitoring device QUV collects several of the results of several similar requests from the quantum computer monitoring device QUV to carry out quantum calculations to the computer core CPU of the computer core CPU, transmitted in response to the rest of the quantum computer QC Quantum computer QC and preferably evaluates them statistically. If the determined statistics of the results of several similar requests from the quantum computer monitoring device QUV transmitted by the computer core CPU to carry out quantum calculations to the computer core CPU of the quantum computer QC deviate from an expected statistic by more than x*σ, the quantum computer monitoring device QUV typically concludes that there is an error in the Quantum Computer QC. Here σ represents the standard deviation of the statistical distribution of the expected response value. Preferably, x is between 1 and 4. Depending on the type of error when executing a quantum computer program, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures.

In the simplest case, exemplary countermeasures can include, for example, resetting and reinitializing the quantum computer QC and/or device parts of the quantum computer QC and/or starting a more extensive self-test program.

A special countermeasure can also be, for example, a translational shift of the substrate D relative to the optical system OS, so that other quantum dots NV1, NV2, NV3 are connected to other core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , C12 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ the previously used quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ replaced. In this case, a reinitialization of the quantum computer QC is unavoidable. In particular, the computer core determines CPU using the methods of DE 10 2020 007 977 B4 the resonance frequencies for controlling and manipulating and entangling the other quantum dots NV1, NV2, NV3 with other core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and preferably stores them in its non-volatile memory NVM and less preferably in its volatile memory RAM. For the translational displacement of the substrate D relative to the optical system OS, the computer core CPU preferably uses the translational positioning device XT of the substrate D in the X direction and the translational positioning device of the substrate D in the Y direction.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to carry out a predetermined quantum computer calculation after carrying out a quantum computer calculation in the first period of time and to transmit the result of the quantum computer calculation back to the quantum computer monitoring device QUV. If the deployable quantum computer QC does not respond within a predetermined time window to the quantum computer monitoring device QUV of the deployable quantum computer QC, there may be an error. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU the control device µC of the deployable quantum computer QC with values that lie within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the execution as incorrect. For this purpose, the quantum computer monitoring device QUV of the deployable quantum computer QC preferably keeps statistical records. If the statistical distribution of the contents of the responses of the computer core CPU of the control device μC of the deployable quantum computer QC does not correspond to an expected statistical distribution, the quantum computer monitoring device QUV of the deployable quantum computer QC preferably also concludes that there is an error. Depending on the type of error, the quantum computer monitoring device QUV of the deployable quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the deployable quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

Such a test typically also checks the correct generation of electromagnetic fields, in particular microwave fields and / or radio wave fields, by a device of the deployable quantum computer QC for manipulating one or more quantum dots NV1, NV2, NV3 in the sense of the document presented here, for example the waveform generator Light source driver LDRV, the light source LD, the microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms (Arbitrary Wave Form Generator) and the microwave and/or radio wave antenna mWA as well as in the broadest sense the Magnetic field generating means MGx, MGy, MGz and the associated magnetic field controls MFSx, MFSy, MFSz as well as the magnetic field sensors MSx, MSy, MSz. Such a test also partly tests the complex and/or real and/or imaginary conductance of a line and the microwave and/or radio wave antenna MWA, which is part of the device of the quantum computer QC for manipulating one or more quantum dots NV1, NV2, NV3 .

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a query message via the internal data bus INTDB to query one or more values of operating voltages of device parts of the quantum computer QC in the second time periods after carrying out a quantum computer calculation in the second time periods and pass it on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a certain error exceeds a permissible value, the quantum computer The QUV quantum computer QC countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to, after carrying out a quantum computer calculation in the first periods, one or more values of current consumption from device parts of the quantum computer QC, from other device parts of the quantum computer QC in the second periods of time and pass it on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

The clock generator OSZ of the computer core CPU of the control device µC of the quantum computer QC typically supplies the computer core CPU of the control device µC of the quantum computer QC with a clock for operating the computer core CPU of the control device µC of the quantum computer QC. The clock generator OSZ of the computer core CPU of the control device μC of the quantum computer QC can also preferably supply further digital circuits and device parts of the quantum computer QC with a clock for operating these digital circuits and device parts of the quantum computer QC.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the processor clock of the computer core CPU of the control device μC of the quantum computer QC and/or its frequency, in particular during or after carrying out a quantum computer calculation in the first time periods and/or the second time period . If an error occurs, such as an incorrect processor clock frequency or a processor clock jitter, the quantum computer monitoring device QUV of the quantum computer QC evaluates the processor clock as incorrect. Thus, the quantum computer monitoring device QUV of the quantum computer QC preferably monitors the clock OSZ of the computer core CPU of the control device μC of the quantum computer QC.

Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible maximum frequency value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

If necessary, the quantum computer monitoring device QUV of the quantum computer QC has its own monitoring clock generation ÜOSZ. Preferably, the monitoring clock generation ÜOSZ of the quantum computer monitoring device QUV of the quantum computer QC typically supplies the quantum computer monitoring device QUV of the quantum computer QC with a clock for operating the quantum computer monitoring device QUV of the quantum computer QC.

For example, the computer core CPU of the quantum computer QC can check the processor clock of the quantum computer monitoring device QUV of the quantum computer QC and/or its frequency and/or the monitoring clock generation ÜOSZ, in particular after carrying out a quantum computer calculation in the second time periods. If an error occurs, such as an incorrect processor clock frequency or a processor clock jitter, the computer core CPU of the quantum computer QC evaluates the processor clock of the quantum computer monitoring device QUV of the quantum computer QC as incorrect. The computer core CPU of the quantum computer QC thus preferably monitors the monitoring clock generation ÜOSZ of the quantum computer monitoring device QUV of the quantum computer QC.

Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

The quantum computer monitoring device QUV preferably has a separate energy supply with preferably a further energy reserve and its own energy processing device. Preferably, the charging device LDV or another additional charging device feeds this additional energy processing device and/or the charging supplies this additional energy reserve. These optional device parts, the further energy reserve, the further energy processing device and the further charging device and possibly a further separation device of the quantum computer monitoring device QUV of the quantum computer QC and their connecting lines are in the 1 no longer shown for better clarity.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the processor input of other device parts of the quantum computer QC and/or their frequency, in particular during or after the execution of a quantum computer calculation in the first time periods and/or the second time period. If an error occurs, such as an incorrect processor clock frequency or processor clock jitter, the quantum computer monitoring device QUV of the quantum computer QC evaluates the relevant processor clock as incorrect. The quantum computer monitoring device QUV of the quantum computer QC thus preferably also monitors the clocks of other device parts of the quantum computer QC. These clocks of other device parts of the quantum computer QC are in the 1 Also not shown for better clarity. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error in the other processor clocks of other device parts of the quantum computer QC exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the light output of the light source LD of the quantum computer QC, in particular after performing a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a query message via the internal data bus INTDB to query one or more values of monitor diodes of the light source LD of the quantum computer QC in the second time periods after performing a quantum computer calculation in the first periods and within one to pass on the specified time window to the quantum computer monitoring device QUV of the quantum computer QC. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check, in particular after carrying out a quantum computer calculation in the second periods, the control of the light source LD of the quantum computer QC by the light source driver LDRV and the functionality of the light source driver LDRV. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to, after performing a quantum computer calculation in the first periods by means of an analog-to-digital converter or the like, one or more values of the operating parameters of the light source driver LDRV and/or or one or more values of the control signals of the light source driver LDRV for the light source LD of the quantum computer QC to be recorded in the second time periods and passed on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the generation of the transmission signal S5 by the waveform generator WFG of the quantum computer QC, in particular after carrying out a quantum computer calculation in the second periods. For this purpose, the quantum computer QC and/or the waveform generator WFG can include a measuring device, for example a digital storage oscilloscope or a similar signal detection device, that records the time course of the transmission signal S5. For example, it can be an analog-to-digital converter that records this signal curve of the transmission signal S5. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to cause the waveform generator WFG of the quantum computer QC to generate a transmission signal S5 in the second time periods after carrying out a quantum computer calculation in the first periods and by means of the Said signal detection device to record the time course of the transmission signal S5. The computer core CPU preferably evaluates the time course of the transmission signal S5 recorded in this way and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request from the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC transmits the detected signal curve of the transmission signal S5 to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV and then the quantum computer monitoring device QUV evaluates the detected signal curve of the transmission signal S5. The response from the computer core CPU should be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the generation of the output signal of the microwave and / or radio wave frequency generator MW / RF-AWFG of the quantum computer QC, in particular after carrying out a quantum computer calculation in the second periods. For this purpose, the quantum computer QC and/or the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC can include a measuring device, for example a digital storage oscilloscope or a similar signal detection device, that measures the time course of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG captured by the quantum computer QC. For example, it can be an analog-to-digital converter that records this signal curve of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to activate the microwave and/or radio wave frequency generator MW/RF-AWFG of the after carrying out a quantum computer calculation in the first periods Quantum computer QC in the second periods to generate an output signal with a specific waveform for test purposes and by means of said signal detection device to record the time course of the output signal of the microwave and / or radio wave frequency generator MW / RF-AWFG of the quantum computer QC. The quantum computer monitoring device QUV of the quantum computer QC can also cause the computer core CPU to use the request message via the internal data bus INTDB to use the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC in the second periods after performing a quantum computer calculation in the first periods To cause the generation of an output signal with a specific waveform for test purposes and to detect the amount and/or phase of the power reflected by the microwave and/or radio wave antenna MWA by means of said signal detection device and thus to the impedance of the microwave and/or radio wave antenna MWA and to close its supply line and record it. The computer core CPU preferably evaluates the time profile of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC and/or the acquired measured values and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC transmits the detected signal curve of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV and then the quantum computer monitoring device QUV the recorded signal curve of the output signal of the microwave and/or radio wave frequency generator MW/RF-AWFG of the quantum computer QC is evaluated. The response from the computer core CPU should be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the data interface DBIF, in particular after carrying out a quantum computer calculation in the second time periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to communicate via the data interface DBIF and the external data bus EXTDB with a higher-level computer system for test purposes in the second after carrying out a quantum computer calculation in the first periods time periods. The higher-level computer system can be, for example, a central control unit ZSE. The higher-level computer system preferably responds with an evaluable answer within a predetermined period of time. The computer core CPU preferably evaluates the message received from the external computer system via the data interface DBIF and the external data bus EXTDB and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request from the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC transmits the message received from the external computer system via the data interface DBIF and the external data bus EXTDB to the quantum computer monitoring device QUV in response to the request from the quantum computer monitoring device QUV and then the quantum computer monitoring device QUV via the Data interface DBIF and the external data bus EXTDB evaluates the message received from the external computer system. The response of the computer core CPU and the higher-level computer system, for example the central control device ZSE, should preferably be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window.

If the computer core CPU does not respond within a predetermined time window after the request is made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that lie within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the execution as incorrect. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the internal data interface MDBIF, in particular after carrying out a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to communicate via the internal data interface MDBIF and the control data bus SDB with an internal computer core of another device part of the quantum computer after performing a quantum computer calculation in the first periods QC to be arranged in the second periods. The internal computer core of the other device part of the quantum computer QC preferably responds with an evaluable answer within a predetermined period of time. The computer core CPU preferably evaluates the message received via the internal data interface MDBIF and the internal data bus INTDB and the control data bus SDB from the internal computer core of the other device part of the quantum computer QC and transmits the result of this evaluation to the quantum computer monitoring device QUV in response to the request of the quantum computer monitoring device QUV. It is also conceivable that the computer core CPU of the quantum computer QC sends the message received via the internal data interface MDBIF and the internal data bus INTDB and the control data bus SDB from the internal computer core of the other device part of the quantum computer QC to the quantum computer monitoring device QUV in response to the request Quantum computer monitoring device QUV is transmitted and then the quantum computer monitoring device QUV evaluates the message received via the internal data interface MDBIF and the internal data bus INTDB and the control data bus SDB from the internal computer core of the other device part of the quantum computer QC. The response of the computer core CPU and the internal computer core of the other device part of the quantum computer QC should preferably be sent to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the amplifier V and the functionality of the photodetector PD, in particular after carrying out a quantum computer calculation in the second periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to cause the light source LD of the quantum computer QC to emit a defined light after performing a quantum computer calculation in the first periods or a test radiation source of the quantum computer QC in the second periods vcause a test light emission to be irradiated, which irradiates the photodetector PD, and/or cause the photodetector PD to generate a test signal for the amplifier V in the second time periods and query the recorded values in the amplifier V and/or operating parameters of the amplifier V and the photodetector PD to be recorded and passed on to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request is made by the quantum computer termonitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that lie within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the execution as incorrect. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

The computer core CPU of the control device µC of the quantum computer QC can typically control the preferably provided test radiation source of the quantum computer QC via the internal data bus interface MDBIF and the internal data bus INTDB and the control data bus SDB. Typically, the control device μC of the quantum computer QC can irradiate the photodetector PD of the quantum computer QC with an optical test signal, for example by means of an optical test radiation source, in order to ensure the functionality of the quantum computer QC. For a better overview, this test radiation source of the deployable quantum computer QC is for irradiating the photodetector PD with test radiation in the 1 not shown.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check temperatures within the quantum computer QC by means of one or more temperature sensors ST, in particular after carrying out a quantum computer calculation in the second time periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to detect one or more temperatures within the quantum computer QC by means of one or more temperature sensors ST of the quantum computer QC after carrying out a quantum computer calculation in the first periods of time and to pass on the recorded temperature measurements to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to, in particular after carrying out a quantum computer calculation in the second periods, check the functionality of the magnetic field sensors MSx, MSy, MSz and/or the functionality of the magnetic field controllers MFSx, MFSy, MFSz and/or the functionality of the Check magnetic field generating means MGx, MGy, MGz. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to perform various quantum computer calculations in the first periods by means of the magnetic field controllers MFSx, MFSy, MFSz and the magnetic field generating means MGx, MGy, MGz of the quantum computer QC to set magnetic flux densities and to record them using the magnetic field sensors MSx, MSy, MSz and to pass on the recorded measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. It can These are the countermeasures or other countermeasures already described in the document presented here.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the first energy processing device SRG and/or the functionality of the second energy processing device SRG2 and/or the functionality of the further energy processing devices, in particular after carrying out a quantum computer calculation in the second time periods. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to set certain supply voltages after carrying out a quantum computer calculation in the first time periods using the first energy processing device SRG and / or the second energy processing device SRG2 and / or the further energy processing devices to adjust and/or modify device parts of the quantum computer QC and, for example, to use measuring devices to adjust their voltage values and/or current values and to pass on the recorded measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the energy reserve BENG and/or the functionality of the second energy reserve BENG2 and/or the functionality of any further energy reserves, if any, of other device parts, in particular after carrying out a quantum computer calculation in the second time periods or already named device parts of the quantum computer QC. For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB, after carrying out a quantum computer calculation in the first periods, by means of charging devices, such as the already named charging device LDV, to check the state of charge of the energy reserve BENG and / or the To change the functionality of the second energy reserve BENG2 and / or the functionality of any further energy reserves, if any, of other device parts and to record the values of the respective current consumption and the voltage curve using suitable measuring means of the quantum computer QC and thus, for example, to draw conclusions about the impedance of these energy reserves. In this case, the quantum computer monitoring device QUV of the quantum computer QC causes the computer core CPU to pass on the recorded measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window using the said request message via the internal data bus INTDB. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with values that are within expected value ranges, the quantum computer monitoring device QUV of the quantum computer QC evaluates the Execution as faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

For example, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU to check the functionality of the separation device TS of the quantum computer QC and the functionality of the loading device LDV of the quantum computer QC, in particular after carrying out a quantum computer calculation in the second periods. Example wise, the quantum computer monitoring device QUV of the quantum computer QC can cause the computer core CPU by means of a request message via the internal data bus INTDB to open the separating device TS after carrying out a quantum computer calculation in the first periods of time and to use the charging devices, such as the already mentioned charging device LDV, to check the charging status of the the energy reserve BENG and/or the functionality of the second energy reserve BENG2 and/or the functionality of any further energy reserves, if any, of other device parts and thereby to record the values of the respective current consumption and the voltage curve using suitable measuring means of the quantum computer QC and to close the separating device TS close and by means of the charging devices, such as the already named charging device LDV, the charge state of the energy reserve BENG and / or the functionality of the second energy reserve BENG2 and / or the functionality of any further energy reserves, if necessary, of other device parts to change again and thereby second values of the respective Current consumption and the voltage curve can be recorded using suitable measuring equipment from the QC quantum computer. In this case, the quantum computer monitoring device QUV of the quantum computer QC causes the computer core CPU to pass on the recorded measured values and second measured values to the quantum computer monitoring device QUV of the quantum computer QC within a predetermined time window via the said request message via the internal data bus INTDB. If the computer core CPU does not respond within a predetermined time window after the request has been made by the quantum computer monitoring device QUV of the quantum computer QC to the computer core CPU of the control device µC of the quantum computer QC with first and second values that lie within expected value ranges, the quantum computer monitoring device QUV evaluates the Quantum computer QC considered the execution to be faulty. Depending on the type of error, the quantum computer monitoring device QUV of the quantum computer QC initiates a countermeasure or changes the database of a statistical evaluation. For example, if the frequency of a specific error exceeds a permissible value, the quantum computer monitoring device QUV of the quantum computer QC initiates countermeasures. These may include the countermeasures already described in the document presented here or other countermeasures.

Quantum computer system QSYS

If the deployable quantum computer QC according to the proposal is integrated into a quantum computer system QUSYS with a second, preferably mobile quantum computer QC2, it is advantageous if a signaling, in particular of a quantum computer calculation result, is sent from the quantum computer QC via at least one signal connection, for example an external data bus EXTDB, to the second Quantum computer QC2 and/or vice versa can be done.

The deployable quantum computer system preferably comprises QUSYS with at least two quantum computers, a first deployable quantum computer QC1 and a second deployable quantum computer QC2, with several measuring devices for recording operating variables of the quantum computer system QUSYS or a device or a system. Typically, the states of the device or system depend on the quantum computer system QUSYS, whereby the first deployable quantum computer QC1 preferably carries out at least twice the same quantum computer calculation that the second deployable quantum computer QC2 carries out. The quantum computer calculation preferably includes a monitoring measure for checking the functionality of the respective deployable quantum computer QC1, QC2. The first deployable quantum computer QC1 preferably carries out the quantum computer calculation of the first deployable quantum computer QC1 independently of the implementation of the quantum computer calculation of the second deployable quantum computer QC2. This makes it possible to compare the results of the quantum computer calculations by the computer cores CPU of the control devices μC of the deployable quantum computers QC1, QC2 and/or the quantum computer monitoring devices QUV of the deployable quantum computers QC1, QC1.

Monitoring procedures

The document presented here also proposes a method for monitoring the execution of a quantum computer program that can be executed on at least one control device µC of a deployable quantum computer QC by means of a quantum computer monitoring device QUV of the quantum computer QC. The deployable quantum computer QC includes quantum dots NV1, NV2, NV3 and preferably core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and the control device µC with the computer core CPU and first means for manipulating quantum dots NV1, NV2, NV3 and, if necessary, for manipulating core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC and second means for reading out the state of quantum dots NV1, NV2, NV3 and, if applicable, core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC. The computer core CPU of the control device µC preferably controls the first means for manipulating quantum dots NV1, NV2, NV3 and possibly core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC and the second means for reading out the state of quantum dots NV1, NV2, NV3 and possibly core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the Quantum Computer QC. The quantum computer monitoring device QUV preferably triggers upon manipulation of a subset of the quantum dots and/or possibly the core quantum dots of the quantum dots NV1, NV2, NV3 and possibly core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the quantum computer QC during the quantum computer program runtime, an exception, in particular an interruption, of the quantum computer program flow, if this manipulation was not intended. This can happen during a program jump due to interference such as cosmic radiation, which is intercepted by this.

The document presented here proposes a non-volatile memory NVM, in particular a read-only memory or a flash memory or a non-volatile memory, for the deployable quantum computer QC, in particular as part of a control unit of a vehicle. A quantum computer program is preferably stored in the non-volatile memory NVM, which can be executed on at least one computer core µC of the quantum computer QC and is suitable for carrying out the method described above.

• Auf dem mindestens einen Rechnerkern CPU der Steuervorrichtung µC soll ein Quantencomputerprogramm ablauffähig sein. Die Quantencomputerüberwachungsvorrichtung QUV überwacht während der Quantencomputerprogrammlaufzeit den Ablauf des Quantencomputerprogramms während der Ausführung durch die anderen Vorrichtungsteile des Quantencomputers QC. Beim einem Zugriff des Rechnerkerns CPU auf einen bestimmten Adressbereich innerhalb eines Speichers RAM, NVM der Steuervorrichtung µC des Quantencomputers QC oder auf andere vorbestimmte Vorrichtungsteile des Quantencomputers QC erzeugt die Quantencomputerüberwachungsvorrichtung QUV eine Ausnahmebedingung (Exception), insbesondere eine Unterbrechung (Interrupt) des Quantencomputerprogrammablaufs. Woraufhin der Rechnerkern CPU der Steuervorrichtung µC des Quantencomputers QC die Ausführung des Quantencomputerprogramms typischerweise in vorzugsweise vorbestimmter Weise unterbricht.

The document presented here proposes the following to further ensure the functionality of the deployable quantum computer QC with at least one computer core CPU, a control device µC and with a quantum computer monitoring device QUV:

• A quantum computer program should be able to run on the at least one computer core CPU of the control device µC. The quantum computer monitoring device QUV monitors the flow of the quantum computer program during execution by the other device parts of the quantum computer QC during the quantum computer program runtime. When the computer core CPU accesses a specific address area within a memory RAM, NVM of the control device µC of the quantum computer QC or other predetermined device parts of the quantum computer QC, the quantum computer monitoring device QUV generates an exception, in particular an interruption of the quantum computer program flow. Whereupon the computer core CPU of the control device μC of the quantum computer QC typically interrupts the execution of the quantum computer program in a preferably predetermined manner.

The computer core CPU of the control device µC or a central control unit ZSE or another computer system, which can be connected, for example, to the computer core CPU of the control device µC of the quantum computer QC via the external data bus EXTDB, can, for example, configure the quantum computer monitoring device QUV. The quantum computer QC and/or the computer core µC preferably has means for running through an exception routine after an exception condition has been triggered during the quantum computer program runtime. The exception routine can itself be a quantum computer program.

Further monitoring procedure

• - Überwachen des korrekten Quantencomputerprogrammablaufs des Quantencomputerprogramms des verlegbaren Quantencomputers QC, insbesondere durch die Quantencomputerüberwachungsvorrichtung QUV oder ein andere Rechnersystem;
• - Durchführen vorbestimmter Quantencomputerberechnungen mit mindestens einer Quantenoperation zur Berechnung vorbestimmter Quantencomputerberechnungsergebnisse in vorbestimmten Zeiträumen vor vorbestimmten Zeitpunkten, insbesondere durch den Quantencomputer QC, und
• - Ansteuern einer Quantencomputerüberwachungsvorrichtung QUV nach diesen vorbestimmten Zeitpunkten und Durchführung eines Rücksetzens (Reset-Funktion) oder Reinitialisierens des Quantencomputers QC auf einen vordefinierten Quantencomputerprogrammrestartzustand oder dergleichen, wenn diese Ansteuerung nicht in vorbestimmter Weise erfolgt durchführt.

The document presented here proposes a method for operating a deployable quantum computer system QUSYS with a deployable quantum computer QC and with a quantum computer monitoring device QUV with the following exemplary steps:

• - Monitoring the correct quantum computer program flow of the quantum computer program of the deployable quantum computer QC, in particular by the quantum computer monitoring device QUV or another computer system;
• - Carrying out predetermined quantum computer calculations with at least one quantum operation for calculating predetermined quantum computer calculation results in predetermined time periods before predetermined times, in particular by the quantum computer QC, and
• - Controlling a quantum computer monitoring device QUV after these predetermined times and carrying out a reset (reset function) or reinitialization of the quantum computer QC to a predefined quantum computer program restart state or the like if this control is not carried out in a predetermined manner.

Data buses

The proposed quantum computer QC preferably includes a data interface DBIF with which the proposed quantum computer QC can communicate with higher-level computer systems du/or other quantum computers QC2 and exchange data. In particular, the proposed quantum computer QC can communicate with a central control unit ZSE via the data interface DBIF and exchange data. The data interface can be wired and/or wireless.

Via the internal data interface MDBIF and the control data bus SDB, the computer core CPU of the control device µC and/or the quantum computer monitoring device QUV with the deployable quantum computer QC can communicate with the device parts of the quantum computer QC and exchange data and signals

Magnetic system

The deployable quantum computer QC preferably includes a system for compensating for external magnetic fields and the earth's magnetic field. For this purpose, the proposed mobile available quantum computer QC preferably has a sensor system for the three-dimensional detection of the three-dimensional vector of the magnetic flux density B. The sensor system for the three-dimensional detection of the three-dimensional vector of the magnetic flux density B preferably detects this three-dimensional vector of the magnetic flux density B in the vicinity of the substrate D. For example, the sensor system for three-dimensional detection of the three-dimensional vector of the magnetic flux density B can include three magnetic field sensors MSx, MSy, MSz for the three spatial directions X, Y, and Z. It is conceivable to use a single sensor system if the alignment of the magnetic field allows it. For example, the quantum computer QC may include a magnetic field sensor MSx for the magnetic flux density B _x in the X-axis direction. For example, the quantum computer QC may include a magnetic field sensor MSy for the magnetic flux density B _y in the Y-axis direction. For example, the quantum computer QC may include a magnetic field sensor MSz for the magnetic flux density B _z in the Z-axis direction.

Typically, the proposed mobile quantum computer QC includes magnetic field generating devices PM, MGx, MGy, MGz. The magnetic field generating devices can include permanent magnets PM and/or coils MGx, MGy, MGz, in particular Helmholtz coils and Helmholtz coil pairs, as magnetic field generating means. The permanent magnets PM permanently generate a magnetic flux density. The coils MGx, MGy, MGz generate a magnetic base density according to their electrical current. The permanent magnets PM and the magnetic field generating means MGx, MGy, MGz are preferably part of a magnetic circuit. Preferably, but not necessarily, the magnetic circuit includes a yoke. The permanent magnet PM is preferably located in an air gap. Preferably, a positioning device PV can reposition the permanent magnet PM relative to the substrate D and/or in the air gap and thus change the magnetic flux density B acting on the substrate D with the quantum dots.

The control device µC of the quantum computer QC preferably comprises a navigation device GPS, which informs the computer core CPU of the control device µC of the current position. The control device μC can preferably use geomagnetic maps of the earth's magnetic field to determine the resulting earth's magnetic field strength and its magnetic flux density component. If the quantum computer QC is moved or rotated translationally, then, for example, the computer core CPU of the quantum computer QC can receive prediction values for future translational coordinates and/or future rotations via the external data bus EXTDB or can predict them from received or determined speed values and rotational speed values. Therefore, the computer core CPU of the quantum computer QC can then make changes to the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ in the future Predict magnetic field and compensate by changing the magnetic field generated in the quantum computer QC using the magnetic field generating devices PM, MGx, MGy, MGz.

• In einem ersten Schritt a) stellt die Steuervorrichtung µC bevorzugt beispielsweise mittels Magnetfaldsensoren MSx, MSy, MSz das derzeit wirkende externe Magnetfeld fest. In einem zweiten Schritt erfasst die Steuervorrichtung µC beispielsweise mittels eines Navigationssystems NAV und/oder einer Positionsermittlungsvorrichtung GPS die aktuellen Koordinaten und/oder die aktuelle Geschwindigkeit und/oder Beschleunigung. Auf Basis dieser Daten und ggf. zusätzlicher Daten, wie zum Beispiel einer elektronischen Karte des Erdmagnetfeldes berechnet beispielsweise die Steuervorrichtung µC des verlegbaren Quantencomputers QC das zu erwartende neue extzerne Magnetfeld und passt bevorzugt die Bestromung der Magnetfelderzeugungsmittel MGx, MGy, MGz so an, dass diese Ändereung des externen Magnetfelds durch die Bewegung des Verlegbaren Quantencomputers QC im Wesentlichen nicht wirksam wird und die Berechnungsergebnisse von Quantencomputerprogrammen des verlegbaren Quantencomputers QC im Wesentlichen nicht beeinflussen.

The method for preventing disruptions to the operation of the deployable quantum computer QC due to changes in external magnetic fields as a result of a movement of the deployable quantum computer QC preferably proceeds as follows:

• In a first step a), the control device μC preferably determines the currently acting external magnetic field, for example using magnetic field sensors MSx, MSy, MSz. In a second step, the control device μC detects the current coordinates and/or the current speed and/or acceleration, for example by means of a navigation system NAV and/or a position determination device GPS. On the basis of this data and possibly additional data, such as an electronic map of the earth's magnetic field, the control device μC of the deployable quantum computer QC, for example, calculates the expected new external magnetic field and preferably adjusts the current supply to the magnetic field generating means MGx, MGy, MGz so that they Change of the external magnetic field through the movement of the relocateable quantum computers QC essentially does not become effective and essentially does not affect the calculation results of quantum computer programs of the deployable quantum computer QC.

To simplify the illustration, we assume here that the navigation device GPS not only determines the translational coordinates, for example the position on the earth's surface, but also the angular orientation of the deployable quantum computer QC and the angular velocity of the change in these angles. Only by taking into account the translational changes and the rotational changes in the position and orientation of the deployable quantum computer QC can the computer system CPU of the deployable quantum computer QC suitably predict the necessary adjustment of the magnetic field generation and suitably control the magnetic field generating devices PM, MGx, MGy, MGz.

For this purpose, the computer core CPU of the control device µC can, for example, cause the first magnetic field controller MFSx to adapt the energization of the first magnetic field generating means MGx, which preferably generates a magnetic flux density B _x , with electrical current.

For this purpose, the computer core CPU of the control device µC can, for example, also cause the second magnetic field controller MFSy to adapt the energization of the second magnetic field generating means MGy, which preferably generates a magnetic flux density B _y , with electrical current. For this purpose, the computer core CPU of the control device µC can, for example, also cause the third magnetic field controller MFSz to adapt the energization of the third magnetic field generating means MGz, which preferably generates a magnetic flux density B _z , with electrical current.

For this purpose, the computer core CPU of the control device µC can, for example, also cause the positioning device PV of the permanent magnet PM to spatially adapt the positioning of the permanent magnet PM, which preferably generates a permanent, spatially inhomogeneous magnetic flux density B, and thus the magnetic flux density at the location of the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

The computer core CPU of the control device µC preferably detects the actual magnetic field using the said magnetic field sensors MSx, MSy, MSz and regulates the magnetic flux density using the actuators described immediately above in the form of the magnetic field generating devices PM, MGx, MGy, MGz in order to avoid deviations between the detected Vector of the magnetic flux density and the desired vector of the magnetic flux density.

The quantum computer QC preferably comprises an acceleration sensor system that can detect translational and/or rotational accelerations and supplies the corresponding values to the computer core CPU of the control device µC of the quantum computer QC, so that it may take countermeasures in the form of counter-accelerations of a position control system not shown in the figures can. If necessary, the computer core CPU of the control device µC of the quantum computer QC can use the positioning device PV of the permanent magnet PM and/or the translational positioning device XT in the X direction and/or the translational positioning device YT in the Y direction for some such countermeasures. The computer core CPU of the control device µC of the deployable quantum computer QC can also, if necessary, modify the focus of the optical system OS depending on such coordinate forecasts and/or speed forecasts and/or acceleration forecasts for translational movements and rotational movements in order to maintain the focus. For example, the computer core CPU of the control device µC of the deployable quantum computer QC can predict deformations and mechanical oscillations within the deployable quantum computer QC on the basis of such coordinate forecasts and/or speed forecasts and/or acceleration forecasts for translational movements and rotational movements and, if necessary. detect and compensate for these using suitable sensors such as cameras and position and distance sensors within the quantum computer QC.

power supply

The deployable quantum computer QC preferably receives its energy from an EV energy supply. A charging device LDV of the energy supply EV receives the energy externally from an energy source PWR.

The book provides a good overview of possible electrical energy sources: Vasily Y. Ushakov (author), “Electrical Power Engineering: Current State, Problems and Perspectives (Green Energy and Technology)”, paperback - August 18, 2018, Springer; 1st ed. 2018 Edition (August 18, 2018), ISBN-10: 3319872850, ISBN-13: 978-3319872858.

This energy source can be, for example, one of the following energy sources:

Electric generator

The energy source can be an electrical generator that converts mechanical energy into electrical energy. The mechanical energy can be, for example, energy transmitted via a wave or the energy of a moving fluid. It can be, for example, an electrical machine, such as a synchronous or asynchronous or direct current motor, a linear motor, a reluctance motor or a BLDC motor or the like, which transfers the mechanical energy of a linear and/or rotational movement by means of induction into lines of a stator and/or or rotor into electrical energy. It can also be a magnetohydrodynamic generator, referred to as an MHD generator for short, which converts the movement of an electrically conductive fluid into electrical energy. The fluid can be a plasma or an electrically conductive liquid, for example a salt solution or a molten metal. The actual energy source can be, for example, a nuclear reactor, an internal combustion engine, a heater, a jet engine, a rocket engine, a ship engine, a Stirling engine, a turbine, a water turbine, a gas turbine, a wind turbine, a tidal power plant, a wave power plant and the like . Magnetohydrodynamic generators, for example, are from the scriptures DE 20 2021 101 169 U1 , WO 2021 159 117 A1 , EP 3 863 165 A1 , US 2021 147 061 A1 , CN 108 831 576 B , US 2019 368 464 A1 , WO 2019 143 396 A2 , EP 3 646 452 B1 , CN 20 634 1126 U , EP 3 279 603 B1 , EP 3 400 642 B1 , EP 3 345 290 B1 , EP 3 093 966 B1 , WO 2016 100 008 A2 , DE 10 2014 225 346 A1 , RU 2014 143 858 A , EP 3 007 350 B1 , US 2016 377 029 A1 , RU 2 566 620 C2 , EP 3 075 064 A1 , EP 2 874 292 B1 , EP 2 986 852 B1 , CN 10 385 5907 B , RU 126 229 U1 , WO 2014 031 037 A2 known. Due to the large number of fonts, the font presented here does not provide a complete list. The document presented here refers to the book Hugo K. Messerle (author), “Magnetohydrodynamic Electrical Power Generation (UNESCO Energy Engineering Series)”, John Wiley & Sons Ltd (August 1, 1995), ISBN-10: 0471942529, ISBN-13 : 978-0471942528.

Electrochemical cell

The energy source can be an electrochemical cell. This can, for example, be an electrochemical cell in the broadest sense, which provides electrical energy through chemical reactions. The document presented includes accumulators, batteries and fuel cells among these electrochemical cells.

Nuclear energy sources

When it comes to nuclear energy sources, the document presented here distinguishes between those that, on the one hand, first convert nuclear energy into mechanical energy, for example using steam cycles and turbines, and then convert it into electrical energy using the generators mentioned above, and on the other hand, nuclear energy convert directly into electrical energy. The document presented here gives examples of betavoltaic cells and thermonuclear generators. These have the advantage that they can be carried out mobile. They therefore fit particularly well with the technical teaching presented here. The radionuclide batteries considered here preferably use the isotopes ⁶⁰ Co, ⁹⁰ Sr, ¹⁰⁶ Ru, ¹⁴⁴ Cs, ¹⁴⁷ Pm, ²¹⁰ Pm, ²¹⁰ Po, ²³⁸ Pu, ²⁴² Cm, ²⁴¹ Am, ²⁴³ Am. The deployable quantum computer QC is preferably protected from radiation from such a nuclear energy source by radiation shielding, for example made of lead. Radionuclide batteries also include betavoltaic cells, which, for example, convert beta radiation from beta emitters directly into electrical energy.

Such radionuclide batteries are, for example, from the scriptures DE 1 240 967 B , DE 1 564 070 B1 , DE 2 124 465 B2 , DE 7 219 216 U , DE 19 782 844 538 B1 , DE 69 411 078 T2 , US 5,443,657 A , US 5,859,484 A , DE 19 602 875 A1 , DE 19 738 066 A1 , DE 19 957 669 A1 , DE 19 957 669 A1 , US 8,552,616 B2 , WO 2009 103 974 A1 and US 2018 226 165 A1 known.

The energy source can also be a renewable energy source such as a solar cell or a hydroelectric power plant with a water turbine and a generator or a wind turbine with a wind turbine and a generator.

The energy source can also be conventional coal, lignite, oil and gas power plants that burn carbonaceous and/or hydrocarbonaceous fuels to generate thermal energy and then convert the thermal energy into mechanical energy and then convert the mechanical energy into electrical energy.

The energy source can be so-called energy harvesting devices. These are devices that use energy differences that already exist in the environment or otherwise, for example from the kinetic energy of a person or another moving object or from thermal differences, for example in heating systems or to obtain the same energy.

Finally, the energy source can simply be the power grid, although the primary energy source can then remain undetermined.

The charging device LDV preferably prepares the energy of the energy supply PWR of the charging device LDV to such an extent that the charging device LDV can charge an energy reserve BENG, BENG2 with the energy of the energy supply PWR. For example, it can be a voltage converter and/or a buck converter or a boost converter or a buck-boost converter depending on the type of power supply PWR. The charging device LDV preferably monitors the charging process of the respective energy reserve BENG, BENG2 when it charges them.

If the quantum computer QC does not execute a quantum computer program and/or does not perform any quantum operations, the charging device LDV can also supply device parts of the deployable quantum computer QC via respective energy processing devices SRG, SRG2. The charging device LDV then preferably also charges one or more of the energy reserves BENG, BENG2 of the deployable quantum computer QC. In the example of the 1 For example, the proposed deployable quantum computer QC has two energy reserves BENG, BENG2 and two energy processing devices SRG, SRG2. The document presented here indicates that the number of energy reserves, energy processing devices and charging devices and separation devices is greater than in the example of 2 can be.

Although the charging device LDV represents a barrier to transients in the power supply PWR, the charging device LDV cannot generally completely suppress these transient disturbances in the power supply PWR. The charging device LDV also produces transient disturbances itself, for example if the charging device LDV is a switching power supply. It has therefore proven useful to have one or more low-noise energy reserves BENG, BENG2 for supplying device parts that are particularly susceptible to interference, such as the photodetector PD, the amplifier V, the light source driver LDRV, the light source LD and, if necessary, for device parts MFSx, MFSy, MFSz, MGx that generate magnetic fields. MGy, MGz and device parts with a particularly time-sensitive signal scheme such as the waveform generator WFG and the microwave and / or radio wave frequency generator MW / RF-AWFG to generate largely freely definable waveforms (English: arbitrary wave form generator). Particularly preferably, these device parts stabilize their internal supply voltages again within these device parts in order to maximally suppress the noise and disturbances in the energy supply. The quantum computer QC preferably comprises one or more energy processing devices SRG, SRG2 for supplying the device parts from the one energy reserve or the plurality of energy reserves BENG, BENG2. The energy processing devices preferably adapt the voltage level that is supplied by the charging device LDV or the energy reserves BENG, BENG2 to the required voltage levels of the device part of the quantum computer QC that is supplied, preferably with a voltage reserve. In a second control stage, which is preferably a linear regulator, these linear regulators can then, for example, use the voltage reserve to adjust the actual supply voltage of the relevant device parts of the quantum computer QC with low noise and precisely.

One or more separating devices TS preferably separate the one charging device or the several charging devices LDV from the one energy processing device or the several energy processing devices SRG, SRG2 and / or the one low-noise energy reserve or from the several low-noise energy reserves BENG, BENG2, if the quantum computer is a Executes quantum computer program and/or performs a quantum operation. A quantum operation in the sense of the document presented here is a manipulation of a quantum dot NV1, NV2, NV3 and/or a core quantum dot CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . In the sense of the document presented here, a quantum computer program is a program that includes at least one quantum operation. One or more binary data in the memory NVN, RAM of the control device μC of the deployable quantum computer QC preferably encode such a quantum operation. For example, it can be a predetermined data word. A quantum operation in the sense of the document presented here manipulates at least the quantum state of at least one quantum dot of the quantum dots NV1, NV2, NV3 of the deployable quantum computer QC and/or manipulates at least the quantum state of at least one core quantum dot of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the deployable quantum computer QC. The technical teaching of the document presented here also refers to the data word that symbolizes such a quantum operation as a quantum op code. A quantum computer program includes at least one quantum op-code. In the above case, if the deployable quantum computer QC is a quantum computer program and / or executes a quantum operation, the one energy reserve or the several energy reserves BENG, BENG2 preferably supply the one energy processing device or the several energy processing devices SRG, SRG2 with electrical energy that is particularly low-noise.

One or more separating devices TS preferably connect the one charging device or the several charging devices LDV with the one energy processing device or the several energy processing devices SRG, SRG2 and / or the one low-noise energy reserve or one of the several low-noise energy reserves BENG, BENG2, if the deployable quantum computer QC does not execute a quantum computer program and/or does not perform a quantum operation. In this case, the charging device LDV preferably charges the one energy reserve or the several energy reserves BENG, BENG2 and, if necessary, supplies the one energy processing device or the several energy processing devices SRG, SRG2 with electrical energy, which typically now has less noise.

Magnetic field shielding

In order to reduce the influence of external magnetic fields, it makes sense if the proposed quantum computer QC is provided with a shield AS for these external magnetic fields. This shielding can be, for example, a passive shielding AS, for example in the form of µ-metal mats, and/or an active shielding AS in the form of a magnetic field-generating system, which generates a magnetic counterfield to an external magnetic interference field and thereby reduces its effect and/or or even compensated. The proposed quantum computer therefore preferably comprises one or more sensors MSx, MSy, MSz for detecting the strength of the magnetic flux density B and/or the magnetic field strength H. The control device preferably uses the μC detected by the one or more sensors MSx, MSy, MSz Values of the magnetic flux density B and/or the magnetic field strength H for controlling magnetic field generating means MGx, MGy, MGz. The magnetic field generating means MGx, MGy, MGz preferably generate a compensating magnetic flux density B of a magnetic counterfield that compensates for the magnetic flux density B of the magnetic interference field.

A first sensor MSx preferably detects the strength of the magnetic flux density B and/or the magnetic field strength H in a first direction, for example an X-axis. A first magnetic field control MFSx preferably supplies a first magnetic field generating means MGx with electrical energy. The first magnetic field generating means MGx preferably generates a magnetic flux density B _x , which preferably essentially has a direction that preferably corresponds to the first direction, for example the direction of the X-axis. The first magnetic field control MFSx preferably supplies the first magnetic field generating means MGx with a first electrical current Ix. The control device µC preferably controls the first magnetic field generating means MGx via the first magnetic field control MFSx. The first magnetic field control MFSx preferably regulates the generation of the magnetic flux density B _x by the first magnetic field generating means MGx in such a way that the magnetic flux density B detected by the first sensor MSx or the magnetic field strength H detected by the first sensor MSx corresponds to a first value. This first value is preferably zero. For this purpose, the first magnetic field controller MFSx evaluates the value of the magnetic flux density B detected by the first sensor MSx or the value of the magnetic field strength H detected by the first sensor MSx.

A second sensor MSy preferably detects the strength of the magnetic flux density B and/or the magnetic field strength H in a second direction, for example a Y-axis. The direction of the Y-axis is preferably chosen perpendicular to the direction of the X-axis. A second magnetic field control MFSy preferably supplies a second magnetic field generating means MGy with electrical energy. The second magnetic field generating means MGy preferably generates a magnetic flux density B _y , which preferably essentially has a direction that preferably corresponds to the second direction, for example the direction of the Y axis. The second magnetic field control MFSy preferably energizes the second magnetic field generating means MGy with a second electrical current Iy. The control device µC preferably controls the second magnetic field generating means MGy via the second magnetic field control MFSy. The second magnetic field control MFSy preferably regulates the generation of the magnetic flux density B _y by the second magnetic field generating means MGy in such a way that the magnetic flux density B detected by the second sensor MSy or the magnetic field strength H detected by the second sensor MSy corresponds to a second value. This second value is preferably zero. For this purpose, the second magnetic field control MFSy evaluates the value of the magnetic flux density B detected by the second sensor MSy or the value of the magnetic field strength H detected by the second sensor MSy.

A third sensor MSz preferably detects the strength of the magnetic flux density B and/or the magnetic field strength H in a third direction, for example a Z axis. The direction of the Z-axis is preferably selected perpendicular to the direction of the X-axis and perpendicular to the direction of the Y-axis. A third magnetic field control MFSz preferably supplies a third magnetic field generating means MGz with electrical energy. The third magnetic field generating means MGz preferably generates a magnetic flux density B _z , which preferably essentially has a direction that preferably corresponds to the third direction, for example the direction of the Z-axis. The third magnetic field control MFSz preferably supplies the third magnetic field generating means MGz with a third electrical current Iz. The control device µC preferably controls the third magnetic field generating means MGz via the third magnetic field control MFSz. The third magnetic field control MFSz preferably regulates the generation of the magnetic flux density B _z by the third magnetic field generating means MGz in such a way that the magnetic flux density B detected by the third sensor MSz or the magnetic field strength H detected by the third sensor MSz corresponds to a third value. This third value is preferably zero. For this purpose, the third magnetic field controller MFSz evaluates the value of the magnetic flux density B detected by the third sensor MSz or the value of the magnetic field strength H detected by the third sensor MSz.

The proposed deployable quantum computer QC typically has an optical system OS that allows the light source LED to irradiate the quantum dots NV1, NV2, NV3 with pump radiation LB. The optical system OS is preferably a confocal microscope. The optical system OS preferably also enables the optical reading of the state of quantum dots NV1, NV2, NV3 of the deployable quantum computer QC. For this purpose, the deployable quantum computer QC of the deployable quantum computer system QUSYS, for example, preferably has a dichroic mirror DBS, which allows the fluorescent radiation FL emitted by the quantum dots NV1, NV2, NV3 to pass and directs the pump radiation LB of the light source LD onto the quantum dots NV1, NV2, NV3 and keeps the pump radiation LB from the photodetector PD for detecting the fluorescence radiation FL. Instead of a dichroic mirror DBS, the deployable quantum computer QC of the quantum computer system QUSYS can, for example, also have a dichroic mirror DBS, which reflects away the fluorescent radiation FL emitted by the quantum dots NV1, NV2, NV3 and the pump radiation LB of the light source LD via the optical system OS onto the quantum dots NV1, NV2, NV3 passes through, so that the pump radiation LB of the light source LD irradiates these quantum dots NV1, NV2, NV3 with pump radiation LB of the pump radiation wavelength λ _pmp . In this case, the optical system OS preferably detects the fluorescence radiation FL of the quantum dots NV1, NV2, NV3 and the dichroic mirror DBS reflects this fluorescence radiation FL onto the photodetector PD for detecting the fluorescence radiation FL. The proposed deployable quantum computer QC therefore comprises, if it uses an optical readout of the states of the quantum dots NV1, NV2, NV3, a photodetector PD for detecting the fluorescence radiation FL of the quantum dots NV1, NV2, NV3. The photodetector PD typically generates a received signal S0 depending on the fluorescence radiation FL. An amplifier V following in the signal path typically amplifies and filters the received signal S0 to an amplified received signal S1. The amplifier V is therefore typically used to amplify and/or filter the output signal of the photodetector PD, which is typically the received signal S0. The amplified received signal S1 is preferably a digitized signal consisting of one or more sample values. The control device μC preferably detects the value of the amplified received signal S1, for example by means of an analog-to-digital converter ADCV. The deployable quantum computer QC according to the proposal includes, if it uses an electronic readout of the states of the quantum dots NV1, NV2, NV3, a corresponding device for electronically reading out the states of the quantum dots NV1, NV2, NV3. At this point the document presented here expressly refers to the document again DE 10 2020 125 189 A1 . These device parts are preferably accommodated in a preferably common housing GH, which is preferably part of the deployable quantum computer QC in the sense of the document presented here. As already described above, the quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are preferably located within said substrate D. The substrate D is preferably doped with dopants. Preferably, the substrate D essentially comprises essentially atoms without a magnetic moment, at least in the effective area of the quantum dots NV1, NV2, NV3. In the case of diamond as the material of the substrate D, the diamond preferably essentially comprises ^1z C isotopes. In the case of using NV centers in diamond as quantum dots, NV1, NV2, NV3 particularly preferably form oxygen atoms ¹⁶ O, ¹⁸ 0 and/or phosphorus and/or sulfur atoms ³² S, ³⁴ S, ³⁶ S without a magnetic moment in the substrate D the doping in the area of the quantum dots NV1, NV2, NV3. This doping in the area of the quantum dots NV1, NV2, NV3 has two tasks. First, these doping atoms change the Fermi level E _F in the region of the quantum dots NV1, NV2, NV3. In the case of using NV centers as quantum dots NV1, NV2, NV3, this doping shifts with the Said doping atoms have the Fermi level E _F in the area of these quantum dots NV1, NV2, NV3. In the case of n-doping, this n-doping shifts the Fermi level E _F in the area of these quantum dots NV1, NV2, NV3 in such a way that the Fermi level is raised and that the NV centers, which are lower in energy, are preferably negatively charged are. The NV centers then represent NV ^- centers. Since NV ^- centers have a magnetic moment of this electron configuration due to the negative charge electron, NV ^- centers are therefore particularly suitable for use as quantum dots NV1, NV2, NV3. Secondly, this doping, which is preferably an n-doping, means that the vacancies in the diamond are electrically charged during the implantation to form the NV centers and therefore do not aggregate due to the electrical repulsion of the negatively charged individual defects . As a result, the concentration of individual defects remains high, which increases the likelihood of NV centers forming when nitrogen is implanted in diamond. The best results are achieved by doping a diamond substrate D with sulfur before nitrogen implantation. Doping with a sulfur isotope without a nuclear magnetic moment is preferred. Such isotopes are the isotopes ³² S, ³⁴ S, ³⁶ S. An alternative is doping with the oxygen isotopes ¹⁶ O, ¹⁸ O, but this is less suitable. It is known that n-doping with phosphr is also said to be successful. However, phosphorus has a nuclear magnetic moment. In principle, N-doping with atoms that have no magnetic nuclear moment makes sense. A shift in the Fermi level E _F by other means, for example by means of preferably very thin electrodes precharged to a suitable potential relative to the substrate D, also led to such effects in advance of the preparation of this document. The substrate D of the deployable quantum computer therefore preferably has a local shift in the Fermi level E _F at least temporarily, so that it is then energetically shifted in such a way that the yield of quantum dots NV1, NV2, NV3 in the form of NV centers during the implantation of the Nitrogen atoms is increased. In an analogous manner, the Fermi level E _F of other substrate materials and/or in relation to other paramagnetic centers (eg the ST1 center) can be influenced in the formation of these paramagnetic centers. Preferably there are the light source LD and the light source driver LDRV and the substrate D and the devices for generating the electromagnetic wave field MW/RF-AWFG, mWA, MGx, MGy, MGz and the control device µC and the memories RAM, NVM of the control device µC and that optical system OS and possibly the amplifier V and the shield AS are located within the housing GH, whereby they are preferably shielded from electromagnetic interference radiation penetrating from outside. For this purpose, the material of the housing GH preferably comprises an electrically conductive material. The housing GH preferably forms a Faraday cage. The material of the housing GH preferably also includes a material for shielding magnetostatic and/or quasi-static magnetic fields. For this purpose, the material of the housing GH preferably comprises so-called µ-metal, which is a particularly soft magnetic material.

The preferred µ-metal (Mumetall, English Mu-metal or English permalloy), proposed here for use in quantum computers QC and quantum technological devices, typically belongs to a group of soft magnetic nickel-iron alloys with 72 to 80% nickel and proportions of copper, Molybdenum, cobalt or chromium with high magnetic permeability, which is used in the proposed deployable quantum computer QC or the proposed quantum technological device for shielding AS from low-frequency external magnetic fields.

According to the proposal, such µ-metal has a high permeability (µ _r =50,000 to 140,000 or more), which causes the magnetic flux of the external low-frequency magnetic fields to concentrate in the material of the housing GH of the deployable quantum computer QC. This effect leads to considerable shielding attenuation when shielding AS from low-frequency or static magnetic interference fields. Thus, the quantum dots NV1, NV2, NV3 and core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are protected against such external magnetic fields even when the deployable quantum computer QC changes the spatial orientation and/or location in the course of a relocation, with such a change in the orientation of the relocatable quantum computer QC and/or the change in location of such a relocatable quantum computer QC typically resulting in a change in the orientation and/or the strength of the magnetic fields act on the deployable quantum computer QC, relative to the deployable quantum computer QC. This is particularly advantageous if the deployable quantum computer QC, for example to save weight, does not have active shielding against external magnetic fields, which would detect the interfering magnetic field using a magnetic field sensor MSX, MSy, MSz and using suitable means MFSx, MFSy, MFSz, MGX, MGy, MGz would generate a magnetic opposing field for compensation.

The document presented here also suggests, among other things, that the shielding AS of the quantum computer ters QC can be part of the housing GH of the deployable quantum computer QC or the housing GH of the deployable quantum computer QC itself. As already described, the control device µC controls the light source LD with the aid of said light source driver LDRV. The control device μC preferably generates a light source control signal, which can be the transmission signal S5, for example, by means of suitable means. The light source driver LDRV then typically supplies the light source LD with electrical energy depending on the light source control signal from the control device μC. The light source LD thus preferably generates the pump radiation LB depending on the light source control signal from the control device μC. Preferably, the light source LD therefore generates the pump radiation LB, preferably depending on the transmission signal S5. In that case the 1 The control device μC transmits the light source control signal preferably via the control data bus SDB and the waveform generator WFG as a transmission signal S5. In the following, the reader can therefore assume, for the sake of simplicity and better understanding, that in the 1 the light source control signal is equal to the transmission signal S5. The light source LD then irradiates the quantum dot or the multiple quantum dots NV1, NV2, NV3 using the optical system OS with pump radiation LB of a pump radiation wavelength λ _pmp . The pump radiation wavelength λ _pmp is preferably between 400 nm to 700 nm wavelength and/or better between 450 nm to 650 nm and/or better between 500 nm to 550 nm and/or better between 515 nm to 540 nm and/or optimally at one wavelength of 532 nm. In the case of NV centers in diamond, a laser diode from Osram of the type PLT5 520B with 520 nm wavelength has proven to be an exemplary source of the pump radiation LB for the irradiation of NV centers in diamond as the material of the substrate D . The quantum dots NV1, NV2, NV3 then emit fluorescence radiation FL with a fluorescence wavelength λ _fl depending on their state and on the pump radiation LB. In the case of NV centers as paramagnetic centers of quantum dots, the <fluorescence wavelength is typically in the range of 638 nm. The intensity I _fl of the fluorescence radiation FL typically depends on the intensity I _pmp of the pump radiation LB and thus also on the light source control signal. The one quantum dot or the multiple quantum dots NV1, NV2, NV3 thus emit fluorescence radiation FL with a fluorescence radiation wavelength X _fl when irradiated with electromagnetic radiation of the pump radiation wavelength λ _pmp . In the case of an optical readout of the state of the quantum dots NV1, NV2, NV3 or the quantum dot, the photodetector PD detects the fluorescence radiation FL by means of the optical system OS and converts the fluorescence radiation FL into a receiver output signal S0. The receiver output signal S0 typically depends on the fluorescent radiation FL striking the photodetector PD. The receiver output signal S0 preferably depends on the intensity I _fl of the fluorescent radiation FL that hits the photodetector PD. In the case of optical reading of the state of the quantum dot(s) NV1, NV2, NV3, the amplifier V amplifies and/or filters the receiver output signal S0 and preferably makes the signal available to the computer core CPU of the control device µC as an amplified received signal S1. The amplifier V preferably stores the values of the sample values of the amplified sample values of the amplified received signal S1, which are digitized by means of an analog-to-digital converter of the amplifier V, in a memory of the amplifier V. The computer core CPU of the control device µC of the deployable quantum computer QC can then query and further process these sample values of the amplified received signal S1 from the memory of the amplifier V, for example via the control data bus SDB. In the case of electronic reading of the quantum dots NV1, V2, NV3 generate in 1 For a better overview, devices HS1 to HS3 and VS1, not shown, for electronically reading out the states of the quantum dots NV1, NV2, NV3 with a control unit B CBB a second received signal. As already described, the control device µC of the deployable quantum computer QC controls the one or more devices for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . By controlling one or more devices (LH1, LH2, LH3, LV1) for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or by controlling the emission of the light source LD, the control device μC of the deployable quantum computer QC can thus control the states of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ ,CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ change and/or link with each other. The control device μC of the deployable quantum computer QC preferably has means for generating a measured value signal with one or more measured values from one or more received signals, in particular from the first received signal and/or the second received signal. Since these received signals depend on the states of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ , the measured value signal typically also depends of states of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

To achieve deployability, the use of a room temperature deployable quantum computer QC based on paramagnetic centers as quantum dots NV1, NV2, NV3 using nuclear magnetic moments as core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ has been used so far , CI3 ₁ , CI3 ₂ , CI3 ₃ with optical pump radiation LB and optical state readout or electronic state readout of the quantum dot states of the quantum dots NV1, NV2, NV3 and a suitable deployable, preferably passive shielding AS proposed.

The proposal presented here now suggests that the deployable quantum computer QC and/or the mobile device has a deployable energy supply EV for supplying the deployable quantum computer QC with energy. This is the only way to complete the installability. The energy supply EV is preferably located within the housing GH. The housing GH can comprise a partial housing with a magnetically shielded area in which the partial devices of the deployable quantum computer QC that are sensitive to magnetic fields are located. Outside this partial housing, but still within the housing GH, there are preferably the parts of the deployable quantum computer QC which, firstly, are not or less sensitive to external magnetic and electromagnetic interference fields and/or themselves generate electromagnetic and/or magnetic interference fields. The energy supply EV is therefore preferably placed outside the partial housing within the housing GH of the deployable quantum computer QC. The quantum computers QC1 to QC16 of a quantum computer system QUSYS can also have a common housing GH.

Typically, the proposed deployable quantum computer QC, together with all the means necessary for its operation, is part of the deployable quantum computer system QUSYS, for example the smartphone or the portable quantum computer system QUSYS or the vehicle or the deployable weapon system.

These means for operating the deployable quantum computer QC must therefore also be deployable. The proposed deployable quantum computer system QUSYS includes deployable means for its operation and in particular one or more deployable energy supplies EV and/or one or more deployable quantum computers QC. For the purposes of this document, these means for operating the deployable quantum computer QC are also part of the smartphone or the item of clothing or the portable quantum computer system QUSYS or the vehicle or the deployable weapon system. It is irrelevant to the interpretation of the claims whether the operation of the deployable quantum computer QC is coupled to means and/or commands outside the quantum computer QC despite the presence of all means for operating the deployable quantum computer QC as part of the deployable quantum computer QC. It is important that the deployable quantum computer QC is potentially functional without these resources and/or commands outside the quantum computer QC. For example, a deployable quantum computer system QUSYS, which waits for an external start command due to the programming of the central control device ZSE and/or the programming of a control device µC of a quantum computer QC of the quantum computer system QUSYS, should still be covered by the claims.

The mobile, deployable energy supply EV preferably comprises one or more deployable charging devices LDV with one or more energy supplies PWR of the charging device en LDV, one or more deployable separation devices TS, one or more deployable energy reserves BENG and one or more deployable energy processing devices SRG. The mobile energy supply EV preferably comprises an energy processing device SRG, in particular a voltage converter or a voltage regulator or a current regulator, which prevents changes in the energy content of the energy reserve BENG of the energy supply EV, for example the state of charge of a battery as an energy reserve BENG of the energy supply EV, from affecting the relocatable quantum computer QC and/or the quantum computer system QUSYS. The mobile energy supply EV supplies the energy processing device SRG with energy and the energy processing device SRG, for example, supplies the deployable quantum computer QC and possibly other parts of the quantum computer system QUSYS with electrical energy. In this case, the energy supply EV, for example, only supplies the quantum computer QC with electrical energy indirectly via the energy processing device SRG.

Typically, according to the proposal, the deployable quantum computer QC is set up and intended to be able to work with a reduced first number of quantum dots NV1, NV2, NV3 even at room temperature. Room temperature as the operating temperature of the quantum dots NV1, NV2, NV3 leads to a broadening of the resonances in the resonance spectrum, so that they overlap. The proposed deployable quantum computer QC therefore preferably has a deployable cooling device KV, which can be deployed together with the deployable quantum computer QC. The relevant relocatable cooling device KV is preferably suitable and/or intended for this purpose is to lower the temperature of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ . Lowering the operating temperature of the quantum dots NV1, NV2, NV3 leads to a narrowing of the resonances in the resonance spectrum, so that they overlap to a lesser extent or not at all. Such cooling by means of a cooling device KV preferably lowers the temperature of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ to this extent that the quantum computer QC can work with a second number of quantum dots NV1, NV2, NV3 that is increased compared to the first number of quantum dots NV1, NV2, NV3.

The deployable quantum computer QC preferably comprises, as the deployable cooling device KV, a closed loop helium gas cooling system HeCLCS, also referred to as closed cycle cryocoolers. For example, we refer to https://en.wikipedia.org/wiki/Cryocooler.

A further embodiment of the proposal concerns a deployable quantum computer that has a deployable second deployable power supply. The relocatable second power supply can be completely or partially identical to the first relocatable power supply (BAT). This second relocatable energy supply BENG preferably supplies the relocatable cooling device KV with energy. This has the advantage that the first energy supply is not disturbed by transient disturbances in the electric motors of the relocatable cooling device KV.

Another embodiment of the proposal concerns a deployable quantum computer QC for use in a mobile device. Use in a smartphone or a portable quantum computer system QUSYS or in a vehicle or in a weapon system is particularly preferred. This means that the document presented here proposes a deployable weapon system with a deployable quantum computer QC, which is part of the deployable weapon system. The use of the deployable quantum computer QC as part of the fire control system of the weapon system or the navigation system GPS, NAV of the weapon system is particularly preferred. The weapon system particularly preferably uses the deployable quantum computer QC to solve NP-complete problems, such as, but not only, the identification of targets, the classification of targets, the assignment of targets to known enemy objects such as aircraft and/or missile types, vehicle types, ship types, Types of missiles, types of floating bodies, types of underwater vehicles, types of underwater objects, types of spacecraft, types of satellites, etc. Furthermore, the selection of the order of attacking the targets and/or the selection of weapons and/or the selection of ammunition for combating the targets can be included Problems that the weapon system solves with the help of the deployable quantum computer QC. In addition, the deployable weapon system can use the deployable quantum computer QC to determine and/or modify and/or monitor the route of the respective projectile or warhead or weapon carrier to the target using the deployable quantum computer QC.

Such a method begins with the acquisition of environmental data by the QUSYS quantum computer system in step A). The environmental data is typically collected using suitable sensors, which can be part of the quantum computer system QUSYS or which are connected to this quantum computer system QUSYS via data connections and transmit environmental data to the quantum computer system QUSYS. In a step B), the quantum computer system QUSYS identifies objects in the environment of the quantum computer system QUSYS, whereby this environment can also be distant from the quantum computer system QUSYS. In step C), the quantum computer system QUSYS classifies the identified objects in the environment of the quantum computer system QUSYS. Typically, in step C), the quantum computer system QUSYS classifies the objects according to danger and/or vulnerability and/or strategic effect in order to maximize a weapon effect. This classification is preferably carried out in step C) using a neural network model, which the quantum computer system QUSYS preferably executes. For this step C), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out the classification of the objects. In a step D, the quantum computer system QUSYS determines the weapons and/or the ammunition and/or the configuration and/or the order of the attacked objects and/or the attacked and/or the non-attacked objects. This determination is preferably carried out in step D) using a neural network model, which the quantum computer system QUSYS preferably executes. In step D), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out these determinations. In one step E) Beats that Quantum computer system QUSYS prefers one or more of these specified attack scenarios to an operator, for example one or more pilots and/or one or more fire control officers or the like. If they give the order to fire, the quantum computer system QUSYS, for example, can implement the released attack scenario in a step F). This is in 12 shown.

The deployable quantum computer QC preferably has a shield AS. The shield AS preferably shields the quantum dots NV1, NV2, NV3, for example the NV centers, against electromagnetic fields and/or electromagnetic waves.

The deployable quantum computer QC preferably comprises an optical system OS that directs the electromagnetic radiation from the light source LD onto the quantum dots NV1, NV2, NV3, for example the paramagnetic centers or the NV centers. The optical system OS preferably includes a confocal microscope.

The optical system OS preferably comprises a first camera CM1, which detects the fluorescence radiation FL of the paramagnetic centers NV1, NV2, NV3 and/or clusters of such paramagnetic centers, for example NV centers and/or clusters of NV centers. Other fluorescent defect centers with other fluorescence wavelengths are conceivable. Such other fluorescent defect centers with other fluorescence wavelengths can thus have fluorescence radiation with a fluorescence wavelength that is different from the fluorescence wavelength λ _fl of the quantum dots NV1, NV2, NV3 and therefore, for example, by means of a dichroic mirror instead of the semi-transparent mirror STM or by means of an optical filter the pump radiation LB and the fluorescence radiation FL of the quantum dots NV1, NV2, NV3 can be optically separated. The substrate D is preferably stored on a positioning table. The positioning table preferably comprises a translational positioning device XT in the X direction and a translational positioning device YT in the Y direction, which preferably controls the control device μC of the quantum computer QC via the control data bus SDB. The first camera CM1 preferably detects the position of the substrate D relative to the optical system OS and thus the position of the quantum dots NV1, NV2, NV3 in the substrate D. The first camera CM1 thus detects the position of the paramagnetic centers, for example the NV centers, relative to the optical system OS. If the substrate D shifts relative to the optical system OS, for example due to mechanical vibrations or other disturbances, an image processing system of the deployable quantum computer QC detects this mechanical displacement, for example by evaluating the position of fluorescent paramagnetic defect centers. The image processing system preferably detects the fluorescence patterns of the defect centers using the first camera CM1 and compares their position on the image with target positions. The image processing system preferably determines a displacement vector and repositions the substrate D using the positioning table XT, YT relative to the optical system OS depending on the determined displacement vector. The image processing device preferably carries out this repositioning in such a way that the position of the quantum dot, for example the paramagnetic center or a cluster of paramagnetic centers, relative to the optical system OS is preferably essentially unchanged after the repositioning has been completed. The image processing system is preferably part of the deployable quantum computer QC. Typically, the controller µC of the quantum computer works as the image processing system. However, the image processing system can also be a separate sub-device of the deployable quantum computer QC. In this case, the control device μC preferably controls the separate image processing system via the control data bus SDB. The image processing system can then be part of the first camera interface CIF, for example. Instead of an image processing system, other position displacement sensors can also detect the displacements of the substrate D relative to the optical system. The proposed quantum computer QC then adjusts the position of the substrate D relative to the optical system OS based on the position displacement data of such position displacement sensors. For example, such position displacement sensors can transmit the detected position displacement data to the control device µC of the quantum computer QC via the control data bus SDB, so that the control device µC of the quantum computer QC, for example depending on this detected position displacement data via the control data bus SDB, moves the positioning table by means of the translational positioning device XT in the X direction and by means of the translational positioning device YT in the Y direction, the control device µC repositions the substrate D relative to the optical system OS depending on this determined position displacement data as if essentially no displacement had taken place. This ensures that the deployable QC quantum computer also works with vibrations, accelerations and the like.

The deployable quantum computer QC preferably comprises a photodetector PD and an amplifier V. The photodetector PD detects the fluorescent radiation FL of the quantum dots NV1, NV2, NV3 when the light source LD irradiates it with its electromagnetic radiation, which serves as pump radiation LB. The deployable quantum computer QC preferably uses this to read out the quantum state of the quantum dots NV1, NV2, NV3. The quantum dots NV1, NV2, NV3 are preferably paramagnetic centers. Quantum dots NV1, NV2, NV3. The paramagnetic centers are preferably NV centers in diamond. The amplifier V amplifies and/or filters the receiver output signal S0 of the photodetector PD to an amplified receiver output signal S1. The amplified receiver output signal can, for example, also be an ordered amount of data in a memory of the amplifier V, the computer core CPU of the control device μC preferably being able to read out this memory of the amplifier V at least partially via the control data bus SDB.

Furthermore, the deployable quantum computer QC can also carry out an electronic readout of quantum dots NV1, NV2, NV3 in parallel or as an alternative to this optical reading of the state of quantum dots NV1, NV2, NV3. For this purpose, the deployable quantum computer QC can have, alternatively or in parallel to the photodetector PD and the amplifier V, a device for electronically reading out the states of the quantum dots NV1, NV2, NV3. The device for electronically reading out the states of the quantum dots NV1, NV2, NV3 preferably comprises electrically conductive lines for applying electric fields in the effective area of the quantum dots NV1, NV2, NV3 and contacts for extracting charge carriers in the area of the quantum dots NV1, NV2, NV3. Furthermore, the device for electronically reading out the states of the quantum dots NV1, NV2, NV3 preferably comprises devices for providing the control signals for controlling said electrically conductive lines for applying electric fields in the effective range of the quantum dots NV1, NV2, NV3. Furthermore, the device for electronically reading out the states of the quantum dots NV1, NV2, NV3 preferably includes devices for amplifying the electrical currents of charge carriers sucked out via the contacts for suctioning off charge carriers in the area of the quantum dots NV1, NV2, NV3. The proposed quantum computer QC preferably has one or more digital-to-analog converters, which are involved in generating the control signals for driving said electrically conductive lines LH1, LH2, LH3, LV1 for applying electric fields in the effective range of the quantum dots NV1, NV2 , NV3 contribute. For controlling the first quantum dot NV1 to be controlled, the first horizontal driver stage HD1 preferably has an analog-to-digital converter, which the computer core CPU of the control device μC can preferably control via the control data bus STB. For controlling the second quantum dot NV2 to be controlled, the second horizontal driver stage HD2 preferably has an analog-to-digital converter, which the computer core CPU of the control device μC can preferably control via the control data bus STB. Preferably, the third horizontal driver stage HD3 has an analog-to-digital converter for controlling the third quantum dot NV3 to be controlled, which the computer core CPU of the control device μC can preferably control via the control data bus STB. The control device µC preferably controls one or more of these digital-to-analog converters via an internal control data bus SDB of the deployable quantum computer QC.

Advantage

Such a deployable quantum computer QC or such a deployable quantum computer system QUSYS enables, at least in some implementations, the solution of NP complete problems in mobile devices. But the advantages are not limited to this.

Features of the proposal

The following list of features reflects the features of the proposal. The features and their sub-features can be combined with each other and with other features and sub-features of this proposal and with features of the description as long as the result of this combination makes sense. In the case of a combination, it is not necessary to include all sub-features of a feature in one feature.

The features are therefore just preferred combinations of characteristics of different examples. The feature references can therefore be expressly changed if it makes sense. They make it easier to rework the proposal. The stress results from the applicable claims.

• - mit einem Substrat D und
• - mit einem oder mehreren Quantenpunkten NV1, NV2, NV3 und
• - mit einer Lichtquelle LD und
• - mit einem Lichtquellentreiber LDRV und
• - mit einer oder mehreren Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes am jeweiligen Ort der Quantenpunkte NV1, NV2, NV3 und
• - mit einer Steuervorrichtung µC und
• - mit einem oder mehreren Speicher RAM, NVM der Steuervorrichtung µC und
• - mit einem Wellenformgenerator WFG und
• - mit einem optischen System OS und
• - mit einer Quantenzustandsauslesevorrichtung,
• - wobei die Quantenzustandsauslesevorrichtung
  • - einen Fotodetektor PD und einem Verstärker V umfassen kann und/oder
  • - eine Vorrichtung zum elektronischen Auslesen der Zustände der Quantenpunkte NV1, NV2, NV3 umfassen kann, und
• - wobei die Quantenpunkte NV1, NV2, NV3 sich in dem Substrat D befinden und
• - wobei das Substrat D dotiert ist, sodass das Fermi-Niveau im Bereich der Quantenpunkte NV1, NV2, NV3 so zu verschoben ist, dass die Quantenpunkte NV1, NV2, NV3 elektrisch geladensind, und
• - wobei insbesondere das Substrat D n-dotiert ist, sodass das Fermi-Niveau im Bereich der Quantenpunkte NV1, NV2, NV3 so angehoben ist, dass die Quantenpunkte NV1, NV2, NV3 negativ elektrisch geladen sind, und
• -- wobei der Wellenformgenerator WFG das Lichtquellensteuersignal S5 erzeugt und
• - wobei der Lichtquellentreiber LDRV die Lichtquelle LD in Abhängigkeit von einem Lichtquellensteuersignal S5 mit elektrischer Energie versorgt und
• - wobei die Steuervorrichtung µC den Wellenformgenerator WFG steuert und
• - wobei die Lichtquelle LD mittels des optischen Systems OS den Quantenpunkt oder die mehreren Quantenpunkte NV1, NV2, NV3 mit Pumpstrahlung LB einer Pumpstrahlungswellenlänge λ_pmp bestrahlt und
• - wobei der eine Quantenpunkt oder die mehreren Quantenpunkte NV1, NV2, NV3 Fluoreszenzstrahlung FL mit einer Fluoreszenzstrahlungswellenlänge λ_fl bei Bestrahlung mit elektromagnetischer Strahlung der Pumpstrahlungswellenlänge λ_pmp emittiert und
• - wobei der Fotodetektor PD mittels des optischen Systems OS zumindest einen Teil der Fluoreszenzstrahlung FL erfasst und ein Empfängerausgangssignal S0 wandelt und wobei der Verstärker V das Empfängerausgangssignal zu einem Empfangssignal S1 verstärkt und filtert und/oder wobei die Vorrichtung zum elektronischen Auslesen der Zustände der Quantenpunkte NV1, NV2, NV3 ein Empfangssignal S1 erzeugt und
• - wobei die Steuereinrichtung µC die einer oder mehreren Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes am jeweiligen Ort der Quantenpunkte NV1, NV2, NV3 steuert und
• - wobei die Steuereinrichtung µC durch Ansteuerung der einer oder mehreren Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes am jeweiligen Ort der Quantenpunkte NV1, NV2, NV3 und/oder durch Steuerung der Emission der Lichtquelle LD Zustände der Quantenpunkte NV1, NV2, NV3 ändern und/oder miteinander verkoppeln kann und
• - wobei die Steuereinrichtung µC über Mittel verfügt, um aus einem oder mehreren Empfangssignalen S1 ein Messwertsignal S4 mit einem oder mehreren Messwerten zu erzeugen und
• - wobei das Messwertsignal S4 von Zuständen von Quantenpunkten NV1, NV2, NV3 abhängt,

gekennzeichnet dadurch

• - dass der verlegbare Quantencomputer und/oder die mobile Vorrichtung eine verlegbare Energieversorgung LDV, TS, BENG, SRG zur Versorgung zumindest eines Teils der Teilvorrichtungen des Quantencomputers mit Energie aufweist und
• - wobei die verlegbare Energieversorgung LDV, TS, BENG, SRG eine mobile Energieversorgung LDV, TS, BENG und eine Energieaufbereitungsvorrichtung SRG, insbesondere einen Spannungswandler oder einen Spannungsregler oder einen Stromregler, aufweist.

Feature 1: Deployable quantum computer in a mobile device, in particular for use in a smartphone or a portable quantum computer system or in a vehicle or in a deployable weapon system,

• - with a substrate D and
• - with one or more quantum dots NV1, NV2, NV3 and
• - with a light source LD and
• - with a light source driver LDRV and
• - with one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and
• - with a control device µC and
• - with one or more memories RAM, NVM of the control device µC and
• - with a waveform generator WFG and
• - with an optical system OS and
• - with a quantum state readout device,
• - where the quantum state readout device
  • - can include a photodetector PD and an amplifier V and/or
  • - a device for electronically reading out the states of the quantum dots NV1, NV2, NV3, and
• - where the quantum dots NV1, NV2, NV3 are located in the substrate D and
• - wherein the substrate D is doped so that the Fermi level in the region of the quantum dots NV1, NV2, NV3 is shifted so that the quantum dots NV1, NV2, NV3 are electrically charged, and
• - where in particular the substrate D is n-doped, so that the Fermi level in the area of the quantum dots NV1, NV2, NV3 is increased so that the quantum dots NV1, NV2, NV3 are negatively electrically charged, and
• -- wherein the waveform generator WFG generates the light source control signal S5 and
• - wherein the light source driver LDRV supplies the light source LD with electrical energy as a function of a light source control signal S5 and
• - wherein the control device µC controls the waveform generator WFG and
• - wherein the light source LD irradiates the quantum dot or the multiple quantum dots NV1, NV2, NV3 by means of the optical system OS with pump radiation LB of a pump radiation wavelength λ _pmp and
• - wherein the one or more quantum dots NV1, NV2, NV3 emit fluorescence radiation FL with a fluorescence radiation wavelength λ _fl upon irradiation with electromagnetic radiation of the pump radiation wavelength λ _pmp and
• - wherein the photodetector PD detects at least part of the fluorescence radiation FL by means of the optical system OS and converts a receiver output signal S0 and wherein the amplifier V amplifies and filters the receiver output signal to a received signal S1 and / or wherein the device for electronically reading out the states of the quantum dots NV1 , NV2, NV3 generates a received signal S1 and
• - wherein the control device µC controls one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and
• - wherein the control device µC by controlling one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and/or by controlling the emission of the light source LD states of the quantum dots NV1, NV2 , NV3 can change and/or link together and
• - wherein the control device µC has means for generating a measured value signal S4 with one or more measured values from one or more received signals S1 and
• - where the measured value signal S4 depends on the states of quantum dots NV1, NV2, NV3,

characterized by this

• - that the deployable quantum computer and/or the mobile device has a deployable energy supply LDV, TS, BENG, SRG for supplying at least some of the sub-devices of the quantum computer with energy and
• - Wherein the relocatable energy supply LDV, TS, BENG, SRG has a mobile energy supply LDV, TS, BENG and an energy processing device SRG, in particular a voltage converter or a voltage regulator or a current regulator.

• - mit einem oder mehreren nuklearen Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ und
• - wobei die eine oder die mehreren Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes am jeweiligen Ort der Quantenpunkte NV1, NV2, NV3 gleichzeitig auch eine oder die mehrere Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes am jeweiligen Ort der Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ sind und
• - wobei die Quantenpunkte NV1, NV2, NV3 und die nuklearen Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ sich in dem gemeinsamen Substrat D befinden und
• - wobei die Steuereinrichtung µC die eine oder die mehreren Vorrichtungen zur Erzeugung eines elektromagnetischen Wellenfeldes steuert und
• - wobei die Steuereinrichtung µC durch Ansteuerung der einer oder mehreren Vorrichtungen zur Erzeugung eines elektromagnetischen Wellenfeldes und/oder durch Steuerung der Emission der Lichtquelle LD
  • - Zustände der Quantenpunkte NV1, NV2, NV3 und/oder Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ ändern kann und/oder
  • - Quantenpunkte NV1, NV2, NV3 mit anderen Quantenpunkten NV1, NV2, NV3 verkoppeln kann und/oder
  • - Quantenpunkte NV1, NV2, NV3 mit Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ verkoppeln kann und/oder
  • - Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ mit anderen Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ verkoppeln kann,
• - dass das Messwertsignal S4 von Zuständen von Quantenpunkten NV1, NV2, NV3 und/oder von Zuständen von Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ abhängt.

Feature 2: Deployable quantum computer according to feature 1,

• - with one or more nuclear quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ and
• - wherein the one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 at the same time also one or more devices mWA, MW/RF-AWFG for generating an electromagnetic wave field at respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ ,CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are and
• - where the quantum dots NV1, NV2, NV3 and the nuclear core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are located in the common substrate D and
• - wherein the control device μC controls the one or more devices for generating an electromagnetic wave field and
• - wherein the control device µC by controlling one or more devices for generating an electromagnetic wave field and / or by controlling the emission of the light source LD
  • - States of the quantum dots NV1, NV2, NV3 and/or core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ can change and/or
  • - Quantum dots NV1, NV2, NV3 can be coupled to other quantum dots NV1, NV2, NV3 and/or
  • - Quantum dots NV1, NV2, NV3 can couple with core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or
  • - Core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ ,CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ with other core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ ,CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ can couple,
• - that the measured value signal S4 depends on states of quantum dots NV1, NV2, NV3 and/or on states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

• - wobei die mobile Energieversorgung LDV, TS, BENG die Energieaufbereitungsvorrichtung SRG, mit Energie versorgt und
• - wobei die Energieaufbereitungsvorrichtung SRG andere Vorrichtungsteile des den Quantencomputers mit elektrischer Energie versorgt.

Feature 3: Deployable quantum computer according to feature 1 or 2,

• - wherein the mobile energy supply LDV, TS, BENG supplies the energy processing device SRG with energy and
• - The energy processing device SRG supplies other device parts of the quantum computer with electrical energy.

• - zum Ersten die Trennvorrichtung TS die Ladevorrichtung LDV mit der Energiereserve BENG verbindet und
• - zum Zweiten die Ladevorrichtung LDV die Energiereserve BENG mit elektrischer Energie einer externen Energieversorgung PWR lädt und/oder

wobei in dem ersten Betriebsmodus

• - zum Ersten die Trennvorrichtung TS die Ladevorrichtung LDV mit der Energieaufbereitungsvorrichtung SRG verbindet und
• - zum Zweiten die Ladevorrichtung LDV die Energieaufbereitungsvorrichtung SRG mit elektrischer Energie einer externen Energieversorgung PWR versorgt und/oder

wobei in dem zweiten Betriebsmodus

• - zum Ersten die Trennvorrichtung TS die Ladevorrichtung LDV von der der Energiereserve BENG trennt und
• - zum Zweiten die Trennvorrichtung TS die Ladevorrichtung LDV von der Energieaufbereitungsvorrichtung SRG trennt und
• - zum Dritten die Energiereserve BENG die Energieaufbereitungsvorrichtung SRG mit elektrischer Energie versorgt.

Feature 4: Deployable quantum computer according to one of features 1 to 3,
wherein the mobile energy supply LDV, TS, BENG has a charging device LDV and a disconnecting device TS and an energy reserve BENG and
wherein the quantum computer has a first operating mode and a second operating mode and
wherein in the first operating mode

• - Firstly, the separating device TS connects the charging device LDV with the energy reserve BENG and
• - Secondly, the charging device LDV charges the energy reserve BENG with electrical energy from an external energy supply PWR and/or

wherein in the first operating mode

• - Firstly, the separating device TS connects the charging device LDV with the energy processing device SRG and
• - Secondly, the charging device LDV supplies the energy processing device SRG with electrical energy from an external energy supply PWR and/or

wherein in the second operating mode

• - Firstly, the separating device TS separates the charging device LDV from the energy reserve BENG and
• - Secondly, the separating device TS separates the charging device LDV from the energy processing device SRG and
• - Thirdly, the energy reserve BENG supplies the energy processing device SRG with electrical energy.

• - mit einem Gehäuse GH und
• - mit einer Abschirmung AS,
• - wobei die Lichtquelle LD und der Lichtquellentreiber LDRV und das Substrat D und die Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung des elektromagnetischen Wellenfeldes und die Steuervorrichtung µC und der Speicher RAM, NVM der Steuervorrichtung µC und das optische System OS und ggf. der Verstärker V und die Abschirmung AS sich innerhalb des Gehäuses GH befinden und
• - wobei die Abschirmung AS Teil des Gehäuses GH oder das Gehäuse GH sein kann und
• - wobei sich zumindest ein Teil der Energieversorgung LDV, TS, BENG, SRG des verlegbaren Quantencomputers QC oder solche Teile der Energieversorgung LDV, TS, BENG, SRG des verlegbaren Quantencomputers QC, die für eine gewisse Zeit eine autonome Energieversorgung für einen autonomen Betrieb des verlegbaren Quantencomputers QC sich innerhalb des gemeinsamen Gehäuses GH befinden.

Feature 5: Deployable quantum computer according to one of features 1 to 4,

• - with a housing GH and
• - with a shielding AS,
• - where the light source LD and the light source driver LDRV and the substrate D and the devices mWA, MW/RF-AWFG for generating the electromagnetic wave field and the control device µC and the memory RAM, NVM of the control device µC and the optical system OS and possibly the Amplifier V and the shield AS are located inside the housing GH and
• - whereby the shielding AS can be part of the housing GH or the housing GH and
• - whereby at least part of the energy supply LDV, TS, BENG, SRG of the deployable quantum computer QC or those parts of the energy supply LDV, TS, BENG, SRG of the deployable quantum computer QC that provide an autonomous energy supply for an autonomous operation of the deployable quantum computer for a certain time Quantum computer QC is located within the common housing GH.

• - wobei eine Energieaufbereitungsvorrichtung SRG und eine Energiereserve BENG der Energieversorgung LDV, TS, BENG, SRG des verlegbaren Quantencomputers QC sich innerhalb der Abschirmung AS befinden.

Feature 6: Deployable quantum computer QC according to feature 5,

• - wherein an energy processing device SRG and an energy reserve BENG of the energy supply LDV, TS, BENG, SRG of the deployable quantum computer QC are located within the shield AS.

• - wobei der verlegbare Quantencomputer QC und alle notwendigen Mitteln zum Betrieb dieses verlegbaren Quantencomputers QC Teil einer mobilen Vorrichtung sind und
• - wobei diese Mittel zum Betrieb des verlegbaren Quantencomputers QC ebenfalls verlegbar sind und wobei diese Mittel zum Betrieb des verlegbaren Quantencomputers QC Teil des Quantencomputers QC sind und
• - wobei diese Mittel zum Betrieb des verlegbaren Quantencomputers QC ebenfalls Teil der mobilen Vorrichtung sind und
• - wobei dabei unerheblich ist, ob der Betrieb des verlegbaren Quantencomputers QC trotz des Vorhandenseins aller Mittel zum Betrieb des verlegbaren Quantencomputers QC als Teil des verlegbaren Quantencomputers QC an Mittel und/oder Kommandos von außerhalb des verlegbaren Quantencomputers QC gekoppelt ist.

Feature 7: Deployable quantum computer QC according to one of features 1 to 6,

• - wherein the deployable quantum computer QC and all the necessary means for operating this deployable quantum computer QC are part of a mobile device and
• - whereby these means for operating the deployable quantum computer QC are also deployable and whereby these means for operating the deployable quantum computer QC are part of the quantum computer QC and
• - whereby these means for operating the deployable quantum computer QC are also part of the mobile device and
• - It is irrelevant whether the operation of the deployable quantum computer QC is coupled to means and/or commands from outside the deployable quantum computer QC despite the presence of all means for operating the deployable quantum computer QC as part of the deployable quantum computer QC.

• - wobei die mobile Vorrichtung insbesondere ein Smartphone oder ein Kleidungsstück oder ein Schmuckstück oder ein tragbares Quantencomputersystem oder ein Fahrzeug oder ein Roboter oder ein Flugzeug oder ein Flugkörper oder ein Satellit oder ein Rumflugkörper oder eine Raumstation oder ein Schwimmkörper oder ein Schiff oder ein Unterwasserfahrzeug oder ein Unterwasserschwimmkörper oder ein verlegbares Waffensystem oder eine andere mobile Vorrichtung ist.

Feature 8: Deployable quantum computer QC according to feature 7,

• - wherein the mobile device is in particular a smartphone or a piece of clothing or a piece of jewelry or a portable quantum computer system or a vehicle or a robot or an aircraft or a missile or a satellite or a rum missile or a space station or a floating body or a ship or an underwater vehicle or a Underwater floating body or a deployable weapon system or other mobile device.

• - wobei der verlegbare Quantencomputer QC eine Positioniervorrichtung XT, YT umfasst und
• - wobei die Positioniervorrichtung XT, YT das Substrat D so gegenüber dem optischen System OS positionieren kann, dass das optische System OS im Zusammenwirken mit der einen oder den mehreren Vorrichtungen mWA, MW/RF-AWFG zur Erzeugung eines elektromagnetischen Wellenfeldes
  • - zum Ersten in einer ersten Positionierung eine erste Menge von Quantenpunkten mit einer ersten Anzahl von Quantenpunkten und ggf. einer zweiten Anzahl von Kernquantenpunkten ansteuern kann und
  • - zum Zweiten in einer zweiten Positionierung eine zweite Menge von Quantenpunkten mit einer dritten Anzahl von Quantenpunkten und ggf. einer vierten Anzahl von Kernquantenpunkten ansteuern kann und
• - wobei die Steuervorrichtung µC die Positioniervorrichtung XT, YT für das Substrat D so steuern kann, dass sie eine erste Positionierung und/oder die zweite Positionierung oder weitere Positionierungen einnehmen kann.

Feature 9: Deployable quantum computer QC according to one of features 1 to 8

• - wherein the deployable quantum computer QC comprises a positioning device XT, YT and
• - Wherein the positioning device XT, YT can position the substrate D relative to the optical system OS in such a way that the optical system OS works in cooperation with the one or more devices mWA, MW/RF-AWFG to generate an electromagnetic wave field
  • - firstly, in a first positioning, can control a first set of quantum dots with a first number of quantum dots and possibly a second number of core quantum dots and
  • - secondly, in a second positioning, can control a second set of quantum dots with a third number of quantum dots and possibly a fourth number of core quantum dots and
• - Wherein the control device μC can control the positioning device XT, YT for the substrate D so that it can assume a first positioning and/or the second positioning or further positioning.

• - wobei der verlegbare Quantencomputer QC einen Temperatursensor ST aufweist, der einen Temperaturmesswert für die Temperatur des Substrats D oder für die Temperatur einer damit thermisch verbundenen Teilvorrichtung des verlegbaren Quantencomputers ermittelt.

Feature 10: Deployable quantum computer QC according to one of features 1 to 9

• - wherein the deployable quantum computer QC has a temperature sensor ST, which determines a temperature measurement value for the temperature of the substrate D or for the temperature of a sub-device of the deployable quantum computer that is thermally connected to it.

• - wobei der verlegbare Quantencomputer QC dazu eingerichtet und vorgesehen ist, mit einer verringerten ersten Anzahl an Quantenpunkten auch bei Raumtemperatur des Substrats D oder einem Temperaturmesswert, der einem Wert größer als 0°C entspricht, arbeiten zu können, und
• - wobei der verlegbare Quantencomputer QC dazu eingerichtet und vorgesehen ist, mit einer erhöhten dritten Anzahl an Quantenpunkten bei einem Temperaturmesswert, der einem Wert kleiner als 0°C entspricht, arbeiten zu können.

Feature 11:Deployable quantum computer QC according to feature 10,

• - wherein the deployable quantum computer QC is set up and intended to be able to work with a reduced first number of quantum dots even at room temperature of the substrate D or a temperature measurement value that corresponds to a value greater than 0 ° C, and
• - wherein the deployable quantum computer QC is set up and intended to be able to work with an increased third number of quantum dots at a temperature measurement value that corresponds to a value less than 0 ° C.

• - wobei der verlegbare Quantencomputer QC dazu eingerichtet und vorgesehen ist, mit einer verringerten zweiten Anzahl an Kernquantenpunkten auch bei Raumtemperatur des Substrats D oder einem Temperaturmesswert, der einem Wert größer als 0°C entspricht, arbeiten zu können, und
• - wobei der verlegbare Quantencomputer QC dazu eingerichtet und vorgesehen ist, mit einer erhöhten vierten Anzahl an Kernquantenpunkten bei einem Temperaturmesswert, der einem Wert kleiner als 0°C entspricht, arbeiten zu können.

Feature 12: Deployable quantum computer QC according to feature 11,

• - wherein the deployable quantum computer QC is set up and intended to be able to work with a reduced second number of core quantum dots even at room temperature of the substrate D or a temperature measurement value that corresponds to a value greater than 0 ° C, and
• - wherein the deployable quantum computer QC is set up and intended to be able to work with an increased fourth number of core quantum dots at a temperature measurement value that corresponds to a value less than 0 ° C.

• - wobei der verlegbare Quantencomputer QC eine oder mehrere verlegbare Kühlvorrichtungen KV aufweist, die zusammen mit dem verlegbaren Quantencomputer QC verlegbar sind, und
• - wobei eine oder mehrere der verlegbaren Kühlvorrichtungen KV dazu geeignet und/oder vorgesehen sind, die Spin-Temperatur von Quantenpunkten NV1, NV2, NV3 und/oder von Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ und/oder die Temperatur des Substrats D zu senken.

Feature 13: Deployable quantum computer QC according to one of features 1 to 12,

• - wherein the deployable quantum computer QC has one or more deployable cooling devices KV, which can be deployed together with the deployable quantum computer QC, and
• - wherein one or more of the deployable cooling devices KV are suitable and/or intended to control the spin temperature of quantum dots NV1, NV2, NV3 and/or of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or to lower the temperature of the substrate D.

• - wobei eine oder mehrere solcher Kühlvorrichtungen KV die Temperatur von Quantenpunkten NV1, NV2, NV3 und/oder die Temperatur von Kernquantenpunkten CI1, CI2, CI3 und/oder die Temperatur des Substrats D soweit senken, dass der verlegbare Quantencomputer QC mit einer gegenüber der verringerten ersten Anzahl an Quantenpunkten NV1, NV2, NV3 erhöhten dritten Anzahl an Quantenpunkten NV1, NV2, NV3 arbeiten kann und/oder
• - wobei eine oder mehrere solcher Kühlvorrichtungen KV die Temperatur von Quantenpunkten NV1, NV2, NV3 und/oder die Temperatur von Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ und/oder die Temperatur des Substrats D soweit senken, dass der Quantencomputer QC mit einer gegenüber der verringerten zweiten Anzahl an Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ mit einer erhöhten vierten Anzahl an Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ arbeiten kann.

Feature 14: Deployable quantum computer QC according to feature 13,

• - Wherein one or more such cooling devices KV reduce the temperature of quantum dots NV1, NV2, NV3 and/or the temperature of core quantum dots CI1, CI2, CI3 and/or the temperature of the substrate D to such an extent that the deployable quantum computer QC has a reduced temperature compared to that first number of quantum dots NV1, NV2, NV3 increased third number of quantum dots NV1, NV2, NV3 can work and / or
• - wherein one or more such cooling devices KV the temperature of quantum dots NV1, NV2, NV3 and / or the temperature of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and/or reduce the temperature of the substrate D to such an extent that the quantum computer QC has a reduced second number of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ can work with an increased fourth number of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ .

• - wobei ein oder mehrere verlegbare Kühlvorrichtungen KV des Quantencomputers QC ein oder mehrere Closed Loop Helium Gas Cooling-Systeme HeCLCS umfassen oder wobei ein oder mehrere verlegbare Closed Loop Helium Gas Cooling Systeme HeCLCS ein oder mehrere verlegbare Kühlvorrichtungen KV umfassen.

Feature 15: Deployable quantum computer QC according to one of features 13 to 14,

• - wherein one or more deployable cooling devices KV of the quantum computer QC comprise one or more closed loop helium gas cooling systems HeCLCS or wherein one or more deployable closed loop helium gas cooling systems HeCLCS include one or more deployable cooling devices KV.

• - wobei der verlegbare Quantencomputer QC eine verlegbare zweite verlegbare Energieversorgung BENG2 aufweist, die von der ersten verlegbaren Energieversorgung BENG verschieden ist, und
• - wobei eine zweite verlegbare Energieversorgung BENG2 ein oder mehrere der verlegbaren Kühlvorrichtungen KV und/oder ein oder mehrere der Closed Loop Helium Gas Cooling-Systeme HeCLCS mit Energie versorgt.

Feature 16: Deployable quantum computer QC according to one or more of the previous features 13 to 15

• - wherein the deployable quantum computer QC has a deployable second deployable energy supply BENG2, which is different from the first deployable energy supply BENG, and
• - wherein a second relocatable energy supply BENG2 supplies one or more of the relocatable cooling devices KV and/or one or more of the closed loop helium gas cooling systems HeCLCS with energy.

• - wobei der verlegbare Quantencomputer QC und/oder die mobile Vorrichtung eine mobilen Datenschnittstelle DBIF, insbesondere eine mobilen Funkdatenschnittstelle und/oder eine drahtgebundene Schnittstelle, aufweist.

Feature 17: Deployable quantum computer QC according to one or more of the previous features 1 to 16,

• - wherein the deployable quantum computer QC and/or the mobile device has a mobile data interface DBIF, in particular a mobile radio data interface and/or a wired interface.

• - wobei ein übergeordnetes System die Steuervorrichtung µC so steuern kann, dass die Steuervorrichtung µC des verlegbaren Quantencomputers QC den verlegbaren Quantencomputer QC zur Durchführung zumindest einer Manipulation eines Quantenzustands zumindest eines Quantenbits der Quantenbits NV1, NV2, NV3 und/oder zur Durchführung zumindest einer Manipulation eines Quantenzustands zumindest eines nuklearen Kernquantenbits der nuklearen Kernquantenbits CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ veranlasst und
• - wobei das übergeordnete System dabei die Steuervorrichtung µC über die mobile Datenschnittstelle DBIF steuert.

Feature 18: Deployable quantum computer QC according to feature 17,

• - wherein a higher-level system can control the control device µC in such a way that the control device µC of the deployable quantum computer QC uses the deployable quantum computer QC to carry out at least one manipulation of a quantum state of at least one quantum bit of the quantum bits NV1, NV2, NV3 and/or to carry out at least one manipulation of a Quantum state of at least one nuclear core quantum bit of the nuclear core quantum bits CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ and
• - The higher-level system controls the control device µC via the mobile data interface DBIF.

• - wobei die erste verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 eine Batterie oder ein Akkumulator oder ein Kondensator oder eine Zusammenschaltung mehrerer dieser Energiespeicher umfassen.

Feature 19: Deployable quantum computer QC according to one or more of the previous features 1 to 18,

• - Wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise a battery or an accumulator or a capacitor or an interconnection of several of these energy storage devices.

• - wobei die erste verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 wiederaufladbare Energiespeicher, insbesondere Akkumulatoren und/oder Kondensatoren und/oder dergleichen, umfassen und
• - wobei der verlegbare Quantencomputer QC und/oder die mobile Vorrichtung eine oder mehrere Ladevorrichtungen LDV aufweist und
• - wobei eine oder mehrere Ladevorrichtungen LDV dazu bestimmt sind und/oder vorgesehen sind zumindest zeitweise in zumindest einigen oder allen der wiederaufladbaren Energiespeicher BENG, BENG2 Energie zu speichern.

Feature 20: Deployable quantum computer QC according to feature 19,

• - wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise rechargeable energy storage devices, in particular accumulators and/or capacitors and/or the like, and
• - wherein the deployable quantum computer QC and/or the mobile device has one or more charging devices LDV and
• - Wherein one or more charging devices LDV are intended and/or are intended to store energy at least temporarily in at least some or all of the rechargeable energy storage devices BENG, BENG2.

• - wobei die ersten verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 einen oder mehrere Energiespeicher umfassen, die jeweils Energie mittels chemischer und/oder elektrochemischer Vorgänge aus zumindest einem oder mehreren Fluiden erzeugen, und
• - wobei die ersten verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 und/oder der verlegbare Quantencomputer QC einen oder mehrere Vorratstanks für diese Fluide umfassen und
• - wobei einer oder mehrere der Vorratstanks die einen oder mehrere der Energiespeicher mit einem oder mehreren dieser Fluide versorgen und
• - wobei einer oder mehrere der Energiespeicher eine oder mehrere galvanische Zellen und/oder eine oder mehrere Brennstoffzellen und/oder eine oder mehrere Verbrennungsmaschinen, die jeweils mit einem oder mehreren elektrischen Generatoren gekoppelt sind, und/oder eine oder mehrere thermische Energieumwandlungsmaschinen, die jeweils mit einem oder mehreren elektrischen Generatoren gekoppelt sind, umfassen und
• - wobei eine oder mehrere der mobilen Energieversorgungen eine oder mehrere Energieaufbereitungsvorrichtungen SRG, insbesondere einen oder mehrere Spannungswandler und/oder einen oder mehrere Spannungsregler und/oder einen oder mehrere Stromregler, aufweisen und
• - wobei einer oder mehrere der Energiespeicher des Quantencomputers QC zumindest zeitweise eine oder mehrere der Energieaufbereitungsvorrichtungen SRG mit Energie versorgen und
• - wobei eine oder mehrere der Energieaufbereitungsvorrichtungen SRG einen oder mehrere Vorrichtungsteile des verlegbaren Quantencomputers QC mit elektrischer Energie versorgen.

Feature 21: Deployable quantum computer QC according to one or more of the previous features 1 to 20,

• - wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy storage devices, each of which generates energy from at least one or more fluids by means of chemical and/or electrochemical processes, and
• - wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 and/or the deployable quantum computer QC comprise one or more storage tanks for these fluids and
• - wherein one or more of the storage tanks supply the one or more of the energy storage devices with one or more of these fluids and
• - wherein one or more of the energy storage devices includes one or more galvanic cells and/or one or more fuel cells and/or one or more combustion engines, each coupled to one or more electrical generators, and/or one or more thermal energy conversion machines, each coupled to one or more electrical generators are coupled, include and
• - wherein one or more of the mobile energy supplies have one or more energy processing devices SRG, in particular one or more voltage converters and / or one or more voltage regulators and / or one or more current regulators, and
• - wherein one or more of the energy storage devices of the quantum computer QC at least temporarily supply one or more of the energy processing devices SRG with energy and
• - Wherein one or more of the energy processing devices SRG supply one or more device parts of the deployable quantum computer QC with electrical energy.

• - wobei die ersten verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 einen oder mehrere Energiespeicher umfassen, die Energie mittels mechanischer Vorgänge erzeugen, und
• - wobei einer oder mehrere dieser Energiespeicher einen oder mehrere Generatoren und/oder eine oder mehrere Lichtmaschinen und/oder einen oder mehrere als Generator betreibbare Elektromotoren umfassen und
• - wobei eine oder mehrere mobile Energieversorgungen des Quantencomputers QC eine oder mehrere Energieaufbereitungsvorrichtungen SRG, insbesondere einen oder mehrere Spannungswandler und/oder einen oder mehrere Spannungsregler und/oder einen oder mehrere Stromregler, aufweisen und
• - wobei einer oder mehrere der Energiespeicher des Quantencomputers QC zumindest zeitweise eine oder mehrere der Energieaufbereitungsvorrichtungen SRG mit Energie versorgen und
• - wobei eine oder mehrere der Energieaufbereitungsvorrichtungen SRG einen oder mehrere Vorrichtungsteile des verlegbaren Quantencomputers QC mit elektrischer Energie versorgen.

Feature 22: Deployable quantum computer QC according to one or more of the previous features 1 to 21,

• - wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy storage devices that generate energy by means of mechanical processes, and
• - wherein one or more of these energy stores comprise one or more generators and/or one or more alternators and/or one or more electric motors that can be operated as a generator and
• - wherein one or more mobile energy supplies of the quantum computer QC have one or more energy processing devices SRG, in particular one or more voltage converters and / or one or more voltage regulators and / or one or more current regulators, and
• - wherein one or more of the energy storage devices of the quantum computer QC at least temporarily supply one or more of the energy processing devices SRG with energy and
• - Wherein one or more of the energy processing devices SRG supply one or more device parts of the deployable quantum computer QC with electrical energy.

• - wobei die erste verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 einen oder mehrere Energiespeicher umfassen, die Energie mittels der Umwandlung elektromagnetischer Strahlung, insbesondere von Licht, in elektrische Energie erzeugen, und
• - wobei einer oder mehrere der Energiespeicher eine oder mehrere Solarzellen oder eine oder mehrere funktionsäquivalente Vorrichtungen, wie beispielsweise PN-Übergänge, umfassen und
• - wobei eine oder mehrere mobile Energieversorgungen des Quantencomputers QC eine oder mehrere Energieaufbereitungsvorrichtungen SRG, insbesondere einen oder mehrere Spannungswandler und/oder einen oder mehrere Spannungsregler und/oder einen oder mehrere Stromregler, aufweisen und
• - wobei einer oder mehrere der Energiespeicher des Quantencomputers QC zumindest zeitweise eine oder mehrere der Energieaufbereitungsvorrichtungen SRG mit Energie versorgen und
• - wobei eine oder mehrere der Energieaufbereitungsvorrichtungen SRG einen oder mehrere Vorrichtungsteile des verlegbaren Quantencomputers QC mit elektrischer Energie versorgen.

Feature 23: Deployable quantum computer QC according to one or more of the previous features 1 to 22,

• - wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy storage devices that generate energy by converting electromagnetic radiation, in particular light, into electrical energy, and
• - wherein one or more of the energy storage devices comprise one or more solar cells or one or more functionally equivalent devices, such as PN junctions and
• - wherein one or more mobile energy supplies of the quantum computer QC have one or more energy processing devices SRG, in particular one or more voltage converters and / or one or more voltage regulators and / or one or more current regulators, and
• - wherein one or more of the energy storage devices of the quantum computer QC at least temporarily one or more of the energy processing devices supply devices SRG with energy and
• - Wherein one or more of the energy processing devices SRG supply one or more device parts of the deployable quantum computer QC with electrical energy.

• - wobei die ersten verlegbare Energiereserve BENG und/oder die zweite verlegbare Energiereserve BENG2 einen oder mehrere Energiespeicher umfassen, die Energie mittels nuklearer Vorgänge erzeugen, und
• - wobei eine oder mehrere der mobilen Energieversorgungen des Quantencomputers QC eine oder mehrere Energieaufbereitungsvorrichtungen SRG, insbesondere einen oder mehrere Spannungswandler und/oder einen oder mehrere Spannungsregler und/oder einen oder mehrere Stromregler, aufweist und
• - wobei einer oder mehrere der Energiespeicher des Quantencomputers QC zumindest zeitweise eine oder mehrere der Energieaufbereitungsvorrichtungen SRG mit Energie versorgen und
• - wobei eine oder mehrere der Energieaufbereitungsvorrichtungen SRG einen oder mehrere Vorrichtungsteile des verlegbaren Quantencomputers QC mit elektrischer Energie versorgen.

Feature 24: Deployable quantum computer QC according to one or more of the previous features 1 to 23,

• - wherein the first deployable energy reserve BENG and/or the second deployable energy reserve BENG2 comprise one or more energy storage devices that generate energy by means of nuclear processes, and
• - wherein one or more of the mobile energy supplies of the quantum computer QC has one or more energy processing devices SRG, in particular one or more voltage converters and / or one or more voltage regulators and / or one or more current regulators, and
• - wherein one or more of the energy storage devices of the quantum computer QC at least temporarily supply one or more of the energy processing devices SRG with energy and
• - Wherein one or more of the energy processing devices SRG supply one or more device parts of the deployable quantum computer QC with electrical energy.

• - wobei der Energiespeicher eine thermonukleare Batterie oder eine funktionsäquivalente Vorrichtung umfasst und

Feature 25: Deployable quantum computer QC according to feature 24,

• - wherein the energy storage comprises a thermonuclear battery or a functionally equivalent device and

• - wobei das Substrat D Diamant umfasst und
• - wobei Quantenpunkte in dem Substrat D Defektzentren und/oder paramagnetische Zentren in Diamant sind.

Feature 26: Deployable quantum computer QC according to one or more of the previous features 1 to 25,

• - wherein the substrate D comprises diamond and
• - where quantum dots in the substrate D are defect centers and / or paramagnetic centers in diamond.

• - wobei Defektzentren in Diamant NV-Zentren oder ST1-Zentren oder SiV-Zentren oder TR12-Zentren sind.

Feature 27: Deployable quantum computer QC according to feature 26,

• - where defect centers in diamond are NV centers or ST1 centers or SiV centers or TR12 centers.

• - mit einem oder mehreren Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃.

Feature 28: Deployable quantum computer QC according to one or more of the previous features 1 to 27,

• - with one or more core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ .

• - wobei die Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ mit Quantenpunkten NV1, NV2, NV3 gekoppelt sind.

Feature 29: Deployable quantum computer QC according to feature 28,

• - where the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are coupled to quantum dots NV1, NV2, NV3.

• - wobei das Substrat D im Wesentlichen zumindest bereichsweise isotopenrein ist und
• - wobei die Isotope des Substrats D abgesehen von Atomen, die die Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ bilden, im Wesentlichen kein magnetisches Kernmoment aufweisen.

Feature 30: Deployable quantum computer QC according to one or more of the two previous features 28 or 29,

• - wherein the substrate D is essentially isotopically pure at least in some areas and
• - wherein the isotopes of the substrate D, apart from atoms that form the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ , have essentially no nuclear magnetic moment.

• - wobei der verlegbare Quantencomputer QC einen oder mehrere Lüfter und/oder einen oder mehrere Wärmetauscher zum Wärmeaustausch mit der Umgebung und/oder einen oder mehrere Wärmetauscher zum Wärmeaustausch mit der Umgebungsluft und/oder einen oder mehrere Strahlungskühler zum Wärmeaustausch mit der Umgebungsluft oder der Umgebung mittels elektromagnetischer Wärmestrahlung aufweist.

Feature 31: Deployable quantum computer QC according to one of features 1 to 30

• - wherein the deployable quantum computer QC has one or more fans and/or one or more heat exchangers for exchanging heat with the environment and/or one or more heat exchangers for exchanging heat with the ambient air and/or one or more radiant coolers for exchanging heat with the ambient air or the environment electromagnetic heat radiation.

• - wobei einer oder mehrere der Lüfter und/oder einer oder mehrere der Wärmetauscher mit einer oder mehrerer der verlegbaren Kühlvorrichtungen KV Energie in Form von Wärme austauschen.

Feature 32: Deployable quantum computer QC according to feature 31 and feature 13

• - Wherein one or more of the fans and/or one or more of the heat exchangers exchange KV energy in the form of heat with one or more of the relocatable cooling devices.

• - mit einer internen Schirmung AS,
• - wobei die interne Schirmung AS das Substrat D mit den Quantenpunkten NV1, NV2, NV3 und ggf. den Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ gegen elektromagnetische Felder der Steuervorrichtung µC und/oder des Speichers RAM, NVM und/oder der Energieversorgung SRG, TS, LDV, BENG, BENG2 und/oder des Lichtquellentreibers LDRV und/oder der Lichtquelle LD abschirmt und/oder
• - wobei die interne Schirmung AS das Substrat D mit den Quantenpunkten NV1, NV2, NV3 und ggf. den Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ anderer Vorrichtungsteile des Quantencomputers QCund/oder gegen Magnetfelder der Steuervorrichtung µC und/oder des Speichers RAM, NVM und/oder der Energieversorgung SRG, TS, LDV, BENG, BENG2 und/oder des Lichtquellentreibers LDRV und/oder der Lichtquelle LD und/oder anderer Vorrichtungsteile des Quantencomputers QC abschirmt

Feature 33: Deployable quantum computer QC according to one or more of the previous features 1 to 32,

• - with an internal shielding AS,
• - where the internal shielding AS is the substrate D with the quantum dots NV1, NV2, NV3 and possibly the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ against electromagnetic Fields of the control device µC and / or the memory RAM, NVM and / or the power supply SRG, TS, LDV, BENG, BENG2 and / or the light source driver LDRV and / or the light source LD shields and / or
• - where the internal shielding AS is the substrate D with the quantum dots NV1, NV2, NV3 and possibly the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of other device parts of the quantum computer QC and/or against magnetic fields of the control device µC and/or the memory RAM, NVM and/or the power supply SRG, TS, LDV, BENG, BENG2 and/or the light source driver LDRV and/or the light source LD and/or other device parts of the Quantum computer QC shields

• - wobei der verlegbare Quantencomputer QC mit einem oder mehreren Rädern oder einem Fahrgestell oder funktionsäquivalenten Vorrichtungsteilen, die auch angetrieben und/oder gebremst sein können, zumindest zeitweise ausgestattet ist.

Feature 34: Deployable quantum computer QC according to one or more of the previous features 1 to 33

• - wherein the deployable quantum computer QC is at least temporarily equipped with one or more wheels or a chassis or functionally equivalent device parts, which can also be driven and / or braked.

• - wobei der verlegbare Quantencomputer QC mit einer oder mehreren Antriebsvorrichtungen zumindest zeitweise ausgestattet ist.
• - wobei es sich bei einem oder mehreren der Antriebsvorrichtungen um ein Rad oder eine Schiffsschraube oder einen Propeller oder eine Turbine oder ein Raketentriebwerk oder ein Antriebsrad oder ein MHD-triebwerk handelt.

Feature 35: Deployable quantum computer QC according to one or more of the previous features 1 to 34,

• - Wherein the deployable quantum computer QC is at least temporarily equipped with one or more drive devices.
• - one or more of the drive devices being a wheel or a propeller or a propeller or a turbine or a rocket engine or a drive wheel or an MHD engine.

• - wobei der verlegbare Quantencomputer QC aerodynamisch geformte Funktionselemente zur Reduzierung und/oder Kontrolle aerodynamischer Effekte und/oder hydrodynamisch geformte Funktionselemente zur Reduzierung und/oder Kontrolle hydrodynamischer Effekte zur Erzeugung eines dynamischen Auftriebs, insbesondere Flügel und /oder Flaps, aufweist.

Feature 36: Deployable quantum computer QC according to one or more of the previous features 1 to 35,

• - wherein the deployable quantum computer QC has aerodynamically shaped functional elements for reducing and/or controlling aerodynamic effects and/or hydrodynamically shaped functional elements for reducing and/or controlling hydrodynamic effects for generating dynamic lift, in particular wings and/or flaps.

• - elektronische Vorrichtungsteile des Quantencomputers QC als Funktionselemente des Quantencomputers QC, zumindest teilweise in strahlenharter Elektronik ausgeführt sind und
• - wobei die Steuervorrichtung µC und/oder der Speicher RAM, NVM der Steuervorrichtung µC und/oder der Rechnerkern CPU und/oder die Datenschnittstelle DBIF und/oder die interne Datenschnittstelle MDBIF und/oder der Lichtquellentreiber LDRV und/oder der Wellenformgenerator WFG und/oder der Verstärker V und/oder der Fotodetektor PD und/oder die erste Kameraschnittstelle CIF und/oder die zweite Kameraschnittstelle CIF2 und/oder die erste Kamera CM1 und/oder die zweite Kamera CM2 und/oder der Temperatursensor ST und/oder der Mikrowellen- und/oder Radiowellenfrequenzgenerator MW/RF-AWFG zur Erzeugung weitestgehend frei vorgebbarer Wellenformen und/oder die Magnetfeldsensoren MSx, MSy, MSz und /oder die Magnetfeldsteuerungen MFSx, MFSy, MFSz und/oder die erste Energieaufbereitungsvorrichtung SRG und/oder die zweite Energieaufbereitungsvorrichtung SRG2 und/oder die Energiereserve BENG und/oder die zweite Energiereserve BENG2 und/oder die Trennvorrichtung TS und/oder die Ladevorrichtung LDV des verlegbaren Quantencomputers solche zumindest teilweise in strahlenharter Elektronik ausgeführten Funktionselemente des Quantencomputers QC sein können und
• - wobei strahlenhart bedeutet, dass diese Funktionselemente des Quantencomputers QC für den Einsatz im Weltraum und/oder in Bereichen erhöhter ionisierender Strahlung, wie beispielsweise Kernreaktoren oder das Umfeld thermonuklearer Batterien vorgesehen und/oder geeignet sind.

Feature 37: Deployable quantum computer QC according to one or more of the previous features 1 to 36

• - Electronic device parts of the quantum computer QC as functional elements of the quantum computer QC, are at least partially designed in radiation-hard electronics and
• - wherein the control device µC and/or the memory RAM, NVM of the control device µC and/or the computer core CPU and/or the data interface DBIF and/or the internal data interface MDBIF and/or the light source driver LDRV and/or the waveform generator WFG and/or the amplifier V and/or the photodetector PD and/or the first camera interface CIF and/or the second camera interface CIF2 and/or the first camera CM1 and/or the second camera CM2 and/or the temperature sensor ST and/or the microwave and /or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms and/or the magnetic field sensors MSx, MSy, MSz and/or the magnetic field controls MFSx, MFSy, MFSz and/or the first energy processing device SRG and/or the second energy processing device SRG2 and/ or the energy reserve BENG and/or the second energy reserve BENG2 and/or the separation device TS and/or the charging device LDV of the deployable quantum computer can be such functional elements of the quantum computer QC that are at least partially implemented in radiation-hard electronics and
• - where radiation-hard means that these functional elements of the quantum computer QC are intended and/or suitable for use in space and/or in areas of increased ionizing radiation, such as nuclear reactors or the environment of thermonuclear batteries.

• - wobei die Steuervorrichtung µC zumindest zeitweise ein neuronales Netzwerkmodell ausführt und
• - wobei das neuronale Netzwerkmodell Eingangswerte und/oder Eingangssignale verarbeitet und
• - wobei das neuronale Netzwerkmodell Ausgangssignale und/oder Ausgangswerte ausgibt und
• - wobei die Steuervorrichtung µC in Abhängigkeit von Ausgangssignalen und/oder Ausgangswerten des neuronalen Netzwerkmodells Zustände von Quantenpunkten NV1, NV2, NV3 und/oder Zustände von Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ beeinflusst und/oder
• - wobei die Steuervorrichtung µC in Abhängigkeit von Zuständen von Quantenpunkten NV1, NV2, NV3 und/oder Zuständen von Kernquantenpunkten CI1₁, CI1₂, CI1₃, CI2₁,CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ Eingangssignale und/oder Eingangswerte des neuronalen Netzwerkmodells beeinflusst.

Feature 38: Deployable quantum computer QC according to one or more of the previous features 1 to 37,

• - wherein the control device µC executes a neural network model at least temporarily and
• - wherein the neural network model processes input values and/or input signals and
• - wherein the neural network model outputs output signals and/or output values and
• - wherein the control device μC determines states of quantum dots NV1, NV2, NV3 and/or states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , _{CI3 1} as a function of output signals and/or output values of the neural network model , CI3 ₂ , CI3 ₃ influenced and/or
• - wherein the control device µC depending on states of quantum dots NV1, NV2, NV3 and / or states of core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ input signals and /or a output values of the neural network model are influenced.

• - wobei der hier vorgelegte Merkmal und die von ihm abhängigen Merkmale alle diese im Folgenden als Fahrzeug bezeichnen und
• - wobei das Fahrzeug einen verlegbaren Quantencomputer QC nach einem oder mehreren der vorhergehenden Merkmale 0 bis 0 umfasst oder
• - wobei der verlegbaren Quantencomputer QC nach einem oder mehreren der vorhergehenden Merkmale 0 bis 0 das Fahrzeug umfasst.

Feature 39: Smartphone and/or a portable quantum computer system and/or a mobile quantum computer system and/or vehicle and/or robot and/or aircraft and/or missile and/or satellite and/or a rum missile and/or space station and/or floating body and /or ship and/or underwater vehicle and/or surface floating body and/or underwater floating body and/or deployable weapon system and/or warhead and/or surface or underwater vehicle and/or projectile and/or other mobile device and/or movable device,

• - the feature presented here and the features dependent on it all hereinafter referred to as a vehicle and
• - wherein the vehicle comprises a deployable quantum computer QC according to one or more of the preceding features 0 to 0 or
• - Wherein the deployable quantum computer QC comprises the vehicle according to one or more of the preceding features 0 to 0.

• - wobei der Quantencomputer QC dazu vorgesehen ist, Datenkommunikation über die Datenschnittstelle DBIF zu entschlüsseln und/oder zu verschlüsseln.

Feature 40: Vehicle according to the previous feature 39

• - Wherein the quantum computer QC is intended to decrypt and/or encrypt data communication via the data interface DBIF.

• - wobei das Fahrzeug Sensoren und/oder Messmittel, die Messwerte über die Umgebung des Fahrzeugs und/oder Zustände des Fahrzeugs und/oder Zustände der Fahrzeuginsassen bzw. Nutzer/Nutzerinnen des Fahrzeugs und/oder Zustände der Zuladung des Fahrzeugs an die Steuervorrichtung µC liefern, umfasst und/oder
• - wobei die Steuervorrichtung µC Messwerte über die Umgebung des Fahrzeugs über die Datenschnittstelle DBIF erhält und/oder
• - wobei der Quantencomputer QC in Abhängigkeit von diesen Messwerten eine Lagebeurteilung für den Gesamtzustand des Fahrzeugs und/oder der Umgebung des Fahrzeugs ermittelt und
• - wobei der Gesamtzustand des Fahrzeugs den Zustand des Umfelds des Fahrzeugs und/oder den Zustand der Fahrzeuginsassen und/oder den Zustand einer Zuladung des Fahrzeugs umfassen kann.

Feature 41: Vehicle according to one or more of the previous features 39 to 40

• - wherein the vehicle has sensors and/or measuring devices which deliver measured values about the surroundings of the vehicle and/or states of the vehicle and/or states of the vehicle occupants or users of the vehicle and/or states of the vehicle's payload to the control device µC, includes and/or
• - wherein the control device µC receives measured values about the surroundings of the vehicle via the data interface DBIF and / or
• - whereby the quantum computer QC determines a situation assessment for the overall condition of the vehicle and/or the surroundings of the vehicle depending on these measured values and
• - Wherein the overall condition of the vehicle can include the condition of the vehicle's surroundings and/or the condition of the vehicle occupants and/or the condition of a payload of the vehicle.

• - wobei zumindest ein Sensor des Fahrzeugs einer der folgenden Messwerte liefernden Sensoren ist oder zumindest einen der folgenden Messwert liefernden Sensoren als Untersystem umfasst:
  • - ein Radar-Sensor und/oder
  • - ein Mikrofon und/oder
  • - ein Ultraschalmikrofon und/oder
  • - einen Ultraschalltransducer und/oder
  • - einen Infrarotsensor und/oder
  • - einen Gassensor und/oder
  • - einen Beschleunigungssensor und/oder
  • - einen Strahlungsdetektor und/oder
  • - ein bildgebendes System und/oder
  • - eine Kamera und/oder
  • - eine Infrarotkamera und/oder
  • - eine Multisprektralkamera und/oder
  • - ein LIDAR-System und/oder
  • - ein Ultraschallmesssystem und/oder
  • - ein Dopplerradarsystem und/oder
  • - ein Quantenradarsystem und/oder
  • - ein Quantensensor und/oder
  • - ein Positionssensor und/oder
  • - ein Navigationssystem und/oder
  • - ein Lagesensor und/oder
  • - ein Partikelzähler und/oder
  • - ein Detektionssystem für biologische Stoffe, insbesondere für biologische Kampstoffe, und/oder
  • - ein Gravimeter und/oder
  • - ein Kompass und/oder
  • - ein Gyroskop und/oder
  • - ein MEMS-Sensor und/oder
  • - ein Drucksensor und/oder
  • - ein Neigungswinkelsensor und/oder
  • - ein Temperatursensor und/oder
  • - ein Feuchtesensor und/oder
  • - ein Windgeschwindigkeitssensor und/oder
  • - ein Wellenfrontsensor und/oder
  • - ein mikrofluidisches Messsystem und/oder
  • - ein Abstandsmesssystem und/oder
  • - ein Längenmesssystem und/oder
  • - ein biologischer Sensor zur Detektion biologischer Marker und/oder Viren und/oder Mikroben oder dergleichen und/oder
  • - ein Sensorsystem zur Erfassung biologischer Messwerte von Fahrzeuginsassen und/oder zur Erfassung biologischer Messwerte lebender Ladung, insbesondere von Tieren und/oder biologischen Materialien,
  • - ein Seat-Occupation-Messystem und/oder
  • - ein Spannungssensor und/oder ein Stromsensor und/oder ein Leistungssensor.

Feature 42: Vehicle according to feature 41

• - wherein at least one sensor of the vehicle is one of the following sensors providing measured values or comprises at least one of the following sensors providing measured values as a subsystem:
  • - a radar sensor and/or
  • - a microphone and/or
  • - an ultrasound microphone and/or
  • - an ultrasound transducer and/or
  • - an infrared sensor and/or
  • - a gas sensor and/or
  • - an acceleration sensor and/or
  • - a radiation detector and/or
  • - an imaging system and/or
  • - a camera and/or
  • - an infrared camera and/or
  • - a multispectral camera and/or
  • - a LIDAR system and/or
  • - an ultrasound measuring system and/or
  • - a Doppler radar system and/or
  • - a quantum radar system and/or
  • - a quantum sensor and/or
  • - a position sensor and/or
  • - a navigation system and/or
  • - a position sensor and/or
  • - a particle counter and/or
  • - a detection system for biological substances, in particular for biological agents, and/or
  • - a gravimeter and/or
  • - a compass and/or
  • - a gyroscope and/or
  • - a MEMS sensor and/or
  • - a pressure sensor and/or
  • - an inclination angle sensor and/or
  • - a temperature sensor and/or
  • - a humidity sensor and/or
  • - a wind speed sensor and/or
  • - a wavefront sensor and/or
  • - a microfluidic measuring system and/or
  • - a distance measuring system and/or
  • - a length measuring system and/or
  • - a biological sensor for detecting biological markers and/or viruses and/or microbes or the like and/or
  • - a sensor system for recording biological measurements of vehicle occupants and/or for recording biological measurements of living cargo, in particular of animals and/or biological materials,
  • - a seat occupation measurement system and/or
  • - a voltage sensor and/or a current sensor and/or a power sensor.

• - wobei der Quantencomputer QC in Abhängigkeit von diesen Messwerten das Fahrzeug und/oder Vorrichtungsteile des Fahrzeugs steuert und/oder eine Steuerung des Fahrzeugs oder eines Vorrichtungsteils des Fahrzeugs beeinflusst.

Feature 43: Vehicle according to feature 41 and/or 42

• - wherein the quantum computer QC controls the vehicle and/or device parts of the vehicle as a function of these measured values and/or influences a control of the vehicle or a device part of the vehicle.

• - wobei das Fahrzeug einen Innenraum aufweist und
• - wobei der Quantencomputer QC in Abhängigkeit von den Messwerten Parameter des Innenraums des Fahrzeugs und/oder ein Vorrichtungsteil im Innenraum des Fahrzeugs beeinflusst.

Feature 44: Vehicle according to feature 43

• - wherein the vehicle has an interior and
• - wherein the quantum computer QC influences parameters of the interior of the vehicle and / or a device part in the interior of the vehicle depending on the measured values.

• - wobei es sich bei dem Fahrzeug um ein Waffensystem handelt und/oder
• - wobei das Fahrzeug ein Waffensystem umfasst, das mit dem Quantencomputer QC gekoppelt ist.

Feature 45: Vehicle according to one or more of the previous features 39 to 44

• - the vehicle is a weapon system and/or
• - Wherein the vehicle includes a weapon system coupled to the quantum computer QC.

• - wobei das Fahrzeug ein Feuerleitsystem umfasst und
• - wobei das Feuerleitsystem den Quantencomputer QC umfasst oder mit dem Quantencomputer gekoppelt ist und
• - wobei die Steuerung des Waffensystems durch das Feuerleitsystem zumindest zeitweise von dem Quantencomputer QC abhängt oder im Zusammenwirken mit dem Quantencomputer QC geschieht.

Feature 46: Vehicle according to feature 45

• - wherein the vehicle includes a fire control system and
• - wherein the fire control system includes the quantum computer QC or is coupled to the quantum computer and
• - whereby the control of the weapon system by the fire control system depends at least temporarily on the quantum computer QC or occurs in cooperation with the quantum computer QC.

• - wobei das Fahrzeug eine Bewertungsvorrichtung umfasst, die die beabsichtigte Steuerung des Waffensystems hinsichtlich der zu erwartenden Wirkungen vor der Ausführung der Steuerung klassifiziert und eine Steuerungsbefehlsklasse ermittelt und
• - wobei die Bewertungsvorrichtung eine Ausführung der Steuerung verhindert oder bis zu einer Freigabe durch einen menschlichen Benutzer aufschiebt, wenn der im Zusammenwirken mit dem Quantencomputer QC ermittelte Steuerungsbefehl in eine vorgegebene Steuerungsklasse fällt.

Feature 47: Vehicle according to features 45 to 46

• - wherein the vehicle comprises an evaluation device which classifies the intended control of the weapon system with regard to the expected effects before the control is carried out and determines a control command class and
• - Wherein the evaluation device prevents execution of the control or postpones it until it is released by a human user if the control command determined in cooperation with the quantum computer QC falls into a predetermined control class.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers QC eine ein oder mehrere Ziele identifiziert.

Feature 48: Vehicle according to features 45 to 48

• - Wherein the vehicle identifies one or more targets with the help of the quantum computer QC.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers QC das eine Ziel oder mehrere Ziele klassifiziert.

Feature 49: Vehicle according to feature 48

• - whereby the vehicle classifies one or more targets with the help of the QC quantum computer.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers QC eine zeitliche Reihenfolge oder Priorisierung der Bekämpfung mehrerer Ziele ermittelt.

Feature 50: Vehicle according to one of features 45 to 49

• - whereby the vehicle uses the quantum computer QC to determine a chronological order or prioritization of combating multiple targets.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers QC einen Zeitpunkt zur Bekämpfung eines Ziels ermittelt.

Feature 51: Vehicle according to one of features 45 to 50

• - The vehicle uses the quantum computer QC to determine a time to attack a target.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers eQC inen Waffentyp und/oder eine Munition zur Bekämpfung eines Ziels ermittelt.

Feature 52: Vehicle according to one of features 45 to 51

• - whereby the vehicle uses the quantum computer eQC to determine a weapon type and/or ammunition to combat a target.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers QC eine Route für das Fahrzeug ermittelt.

Feature 53: Vehicle according to one of features 39 to 52

• - whereby the vehicle determines a route for the vehicle with the help of the quantum computer QC.

• - wobei das Fahrzeug mit Hilfe des Quantencomputers QC eine Route für das eine Waffe oder einen Gefechtskopf oder ein Geschoss oder eine Munition oder ein anderes Fahrzeug ermittelt.

Feature 54: Vehicle according to one of features 45 to 52

• - whereby the vehicle uses the quantum computer QC to determine a route for a weapon or a warhead or a projectile or an ammunition or other vehicle is identified.

• - wobei die Steuervorrichtung µC zumindest zeitweise ein neuronales Netzwerkmodell ausführt und
• - wobei das neuronale Netzwerkmodell Eingangswerte und/oder Eingangssignale verarbeitet und
• - wobei das neuronale Netzwerkmodell Ausgangssignale und/oder Ausgangswerte ausgibt und
• - wobei die Steuervorrichtung µC in Abhängigkeit von Ausgangssignalen und/oder Ausgangswerten des neuronalen Netzwerkmodells Zustände der Quantenpunkte NV1, NV2, NV3 und/oder Zustände der Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ beeinflusst und/oder
• - wobei die Steuervorrichtung µC in Abhängigkeit von Zuständen der Quantenpunkte NV1, NV2, NV3 und/oder Zuständen der Kernquantenpunkte CI1₁, CI1₂, CI1₃, CI2₁, CI2₂, CI2₃, CI3₁, CI3₂, CI3₃ Eingangssignale und/oder Eingangswerte des neuronalen Netzwerkmodells beeinflusst.

Feature 55: Vehicle according to one or more of features 39 to 54

• - wherein the control device µC executes a neural network model at least temporarily and
• - wherein the neural network model processes input values and/or input signals and
• - wherein the neural network model outputs output signals and/or output values and
• - wherein the control device μC determines states of the quantum dots NV1, NV2, NV3 and/or states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , _{CI3 1} as a function of output signals and/or output values of the neural network model , CI3 ₂ , CI3 ₃ influenced and/or
• - wherein the control device µC depending on states of the quantum dots NV1, NV2, NV3 and/or states of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ input signals and /or input values of the neural network model are influenced.

List of characters

• 1 shows the quantum computer QC described above in a simplified schematic form.
• 2 shows two exemplary quantum bits QUB1, QUB2.
• 3 shows the block diagram of an exemplary quantum computer QC with an exemplary, schematically indicated three-bit quantum register.
• 4 shows an exemplary quantum computer system QUSYS with an exemplary central control unit ZSE.
• 5 shows an exemplary aircraft FZ as an exemplary vehicle with several deployable quantum computers QC1, QC2.
• 6a shows another example of the use of the proposed deployable quantum computer QC in an aircraft FZ.
• 6b shows a deployable quantum computer QC in a sea container SC on a low-loader TL with a tractor ZM.
• 6c shows an exemplary aircraft carrier FZT as an exemplary floating body.
• 6d shows a factory hall FHB as an example of a stationary device into which several deployable quantum computers QC were installed.
• 7 shows another example of a vehicle with a proposed quantum computer system QUSYS with here, for example, two quantum computers QC, which is an exemplary submarine SUB.
• 8th shows a vehicle with a first quantum computer QC1, a second quantum computer QC2, a central control unit ZSE and an external data bus EXTDB, which connects them to a quantum computer system QUSYS, the vehicle being in the example 8th an exemplary motor vehicle is a motor vehicle.
• 9 shows a check whether the solution to an NP-complete problem is actually a solution.
• 10 shows a quantum computer system QUSYS with a daisy chain arrangement of quantum computers QC1 to QC16.
• 11 shows a quantum computer system QUSYS with several sub-quantum computer systems.
• 12 shows the solution of an NP-complete problem using a mobile deployable quantum computer QC.
• 13 shows an exemplary structure of an amplifier V, as shown in the 1 is marked.
• 14 shows an example of a garment with a deployable quantum computer system QUSYS.
• 15 shows an example of a satellite or spacecraft as an example of a vehicle with a deployable quantum computer system QUSYS.
• 16 shows an example of a smartphone with a deployable QUSYS quantum computer system.

Description of the characters

The figures explain the proposal schematically and simplified. The disclosure of the document presented here is not limited to the figures and also includes other combinations.

Figure 1

1 shows the exemplary deployable quantum computer QC described above in a schematically simplified form. The document presented here ver avoid repeating the description here.

Figure 2

The 2 shows two exemplary quantum bits QUB1, QUB2. In the following, the document presented here first describes the first quantum bit QUB1. The second quantum bit QUB2 results analogously. The substrate D has a bottom US on which a back contact BSC is attached. The substrate D is particularly preferably made of diamond. The quantum dots NV1, NV2, NV3 and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , _{CI3 2 ,} CI3 ₃ are preferably irradiated with pump radiation LB from the underside US of the substrate D The isotopes of the substrate D preferably have essentially no nuclear magnetic moment μ. An epitaxial layer DEPI is applied to the substrate D to improve the electronic properties. Preferably, the substrate D and/or the epitaxial layer DEPI essentially only comprise isotopes without a nuclear magnetic moment μ. Preferably, the substrate D and/or the epitaxial layer DEPI essentially comprises only one isotope type of an isotope without a nuclear magnetic moment μ. The package consisting of substrate D and epitaxial layer DEPI has a surface OF. A vertical line LV1 is applied to the surface OF as part of an exemplary crossbar structure, through which a vertical electrical current IV1 modulated with a vertical modulation flows. The surface OF and the vertical line LV1 are covered by insulation IS. If necessary, there is further insulation between the vertical line LV1 and the surface OF in order to electrically isolate the vertical line LV1. A first horizontal line LH1 is applied to the insulation IS, through which a first horizontal electrical current IH1, modulated with a first horizontal modulation, flows. The first vertical line LV1 and the first horizontal line LH1 are preferably electrically insulated from each other. Preferably, the angle α ₁₁ between the first horizontal line LH1 and the first vertical line LV1 is a right angle of 90°. The first horizontal line LH1 and the first vertical line LV1 preferably cross above the paramagnetic center of the first quantum dot NV1. The first quantum dot NV1 is preferably an NV center in diamond. The first quantum dot NV1 is preferably located directly below the intersection point of the first horizontal line LH1 with the first vertical line LV1 at a first distance d1 below the surface OF in the epitaxial layer DEPI. The first distance d1 is preferably between 10µm and 20µm, worse between 5µm and 40µm, worse between 2.5µm and 80µm. In the case of diamond as the material of the epitaxial layer DEPI, the first quantum dot NV1 can be, for example, an NV center. The use of SiV and/or TR12 centers and other paramagnetic centers in diamond is also conceivable. If the horizontal modulation of the first horizontal current IH1 is shifted by +/- π/2 compared to the vertical modulation of the first vertical current IV1, then at the location of the first quantum dot NV1, for example, a rotating magnetic field B _NV results, which influences the first quantum dot NV1 . The control device µC of the quantum computer QC can use this to manipulate the first quantum dot NV1. Here, the control device µC selects the frequency so that the first quantum dot NV1 resonates with the rotating magnetic field B _NV . The duration of the pulse then determines the angle of rotation of the quantum information of the first quantum dot NV1. The direction of polarization determines the direction.

The 2 includes, for example, six core quantum dots
firstly, a first core quantum dot CI1 ₁ , which is assigned to the first quantum dot NV1, and
secondly, a second core quantum dot CI1 ₂ , which is assigned to the first quantum dot NV1, and
thirdly, a third core quantum dot CI1 ₃ , which is assigned to the first quantum dot NV1, and
fourthly, a first core quantum dot CI2 ₁ which is assigned to the second quantum dot NV2, and
fifth, a second core quantum dot CI2 ₂ associated with the second quantum dot NV2, and
sixthly, a third core quantum dot CI2 ₃ which is assigned to the second quantum dot NV2.

Each of the core quantum dots forms a core quantum bit with the lines LV1, LH1, LH2. In the respective core quantum bit, the quantum dot NV1, NV2 is replaced by the core quantum dot CI1 ₁ , CI1 ₂ , CI1 ₃ in QUB1 and CI2 ₁ , CI2 ₂ , CI2 ₃ in QUB2.

Isotopes with a magnetic nuclear spin preferably form the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ in the substrate D. In the case of diamond as the material of the epitaxial layer DEPI or the substrate D, a core quantum dot can, for example be a ¹³ C isotope or a nucleus of a nitrogen atom of a NV center.

2 shows an exemplary quantum register with a first quantum bit QUB1 and a second quantum bit QUB2. The quantum bits QUB1, QUB2 of the quantum register have a common substrate D and a common epitaxial Layer DEPI. The first vertical line of the first quantum bit QUB1 is the first vertical line LV1 of the second quantum bit QUB2. The first vertical line LV1 and the first horizontal line LH1 preferably cross above the first quantum dot NV1, which is preferably located at a first distance d1 below the surface OF, at a preferably right angle α ₁₁ of 90°. The first vertical horizontal line LV1 and the second horizontal line LH2 preferably cross above the second quantum dot NV2, which is preferably located at a second distance d2 below the surface, at a preferably right angle α ₁₂ . The first distance d1 and the second distance d2 are preferably similar to one another. For NV centers in diamond as quantum dots NV1, NV2, these distances d1, d2 are preferably 10nm to 20nm. A first vertical current IV1 modulated with a horizontal modulation flows through the first vertical line LV1. A first horizontal current IH1 modulated with a first horizontal modulation flows through the first horizontal line LH1. A second horizontal current IH2 modulated with a second horizontal modulation flows through the second horizontal line LH2. The first quantum dot NV1 is spaced from the second quantum dot NV2 by a distance sp12.

The 2 shows an exemplary core-electron core-electron quantum register CECEQUREG.

The core-electron-core-electron quantum register includes an electron-electron quantum register in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the second quantum dot NV2 of the second quantum bit QUB2.

The core-electron-core-electron quantum register includes a first core-electron quantum register, in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the first core quantum dot CI1 ₁ of the first core quantum bit.

The core-electron-core-electron quantum register includes a second core-electron quantum register, in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the second core quantum dot CI1 ₂ of the second core quantum bit.

The core-electron-core-electron quantum register includes a third core-electron quantum register, in which the first quantum dot NV1 of the first quantum bit QUB1 can couple with the third core quantum dot CI1 ₃ of the second core quantum bit.

The core-electron-core-electron quantum register includes a fourth core-electron quantum register, in which the second quantum dot NV2 of the second quantum bit QUB2 can couple with the first core quantum dot CI2 ₁ of the fourth core quantum bit.

The core-electron-core-electron quantum register includes a fifth core-electron quantum register, in which the second quantum dot NV2 of the second quantum bit QUB2 can couple with the second core quantum dot 1, CI2 ₂ of the fifth core quantum bit.

The core-electron-core-electron quantum register includes a sixth core-electron quantum register, in which the second quantum dot NV2 of the second quantum bit QUB2 can couple with the third core quantum dot CI2 ₃ of the sixth core quantum bit.

This is the simplest form of a quantum bus with a first quantum ALU QUALU1 (NV1, CI1 ₁ , CI1 ₂ , CI1 ₃ ) and a second quantum ALU QUALU2 (NV2, CI2 ₁ , CI2 ₂ , CI2 ₃ ). The control device μC can entangle the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU NV1, CI1 ₁ , CI1 ₂ , CI1 ₃ and the core quantum dots of the second quantum ALU QUALU2 with one another using the first quantum dot NV1 and the second quantum dot NV2. The first quantum dot NV1 and the second quantum dot NV2 are preferably used to transport the dependency and the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ are used for calculations and storage. This takes advantage of the fact that the range of coupling of the quantum dots NV1, NV2 with each other is greater than the range of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ with each other and that the T2 time of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ is longer than that of the quantum dots NV1, NV2.

Typically, the distance between the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU QUALU1 and the second quantum dot NV2 is greater than the electron-nucleus coupling range, so that the state of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU QUALU1 cannot influence the state of the second quantum dot NV2 and the state of the second quantum dot NV2 cannot influence the state of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ of the first quantum ALU QUALU1.

Typically, the distance between the core quantum dots CI2 ₁ , CI2 ₂ , CI2 ₃ of the second quantum ALU QUALU2 and the first quantum dot NV1 is greater than the electron-nucleus coupling range, so that the state of Core quantum dots CI2 ₁ , CI2 ₂ , CI2 ₃ of the second quantum ALU QUALU2 cannot influence the state of the first quantum dot NV1 and the state of the first quantum dot NV1 cannot directly influence the state of the core quantum dots CI2 ₁ , CI2 ₂ , CI2 ₃ of the second quantum ALU QUALU2.

2 shows an exemplary quantum register with a second horizontal shielding line SH2 and with a first horizontal shielding line SH1 and with a third horizontal shielding line SH3. The additional shielding lines allow the injection of additional currents to improve the selection of the quantum dots during the execution of the operations by energizing the vertical and horizontal lines. The two additional lines enable even better adjustment.

2 shows an exemplary two-bit electron-electron quantum register with a common first vertical line LV1, several shield lines and two quantum dots NV1, NV2. In the 2 To explain the readout process, a first vertical shielding line SV1 is drawn parallel to the first vertical line LV1. Since this is a cross-sectional image, the corresponding second vertical shielding line SV2, which also runs parallel to the first vertical line LV1 on the other side, is not shown. In this example, the shielding lines are connected to the substrate D via contacts. If an extraction field is now created between two parallel shielding lines by applying an extraction voltage between these shielding lines SV1, SV2, a measurable current flow occurs when the light source LD irradiates the quantum dots NV1, NV2 with pump radiation LB and these are in the correct quantum state. Further information can be found, for example, in Petr Siyushev, Milos Nesladek, Emilie Bourgeois, Michal Gulka, Jaroslav Hruby, Takashi Yamamoto, Michael Trupke, Tokuyuki Teraji, Junichi Isoya, Fedor Jelezko, “Photoelectrical imaging and coherent spin-state readout of single nitrogen-vacancy centers in diamond”, Science 363, 728-731 (2019) 15 February 2019 can be found.

The two quantum dots NV1, NV2 2 are each part of several nuclear-electron quantum registers. Each quantum dot NV1, NV2 is the in the example 2 Part of a respective quantum ALU QUALU1, QUALU2.

The first quantum dot NV1 of the first quantum ALU QUALU1 can be used in the example 2 interact with a first core quantum point CI1 ₁ of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the first horizontal line LH1 and the first vertical line LV1 with a first horizontal current IH1 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a first electron nuclear radio wave resonance frequency f _{RWEC1_1} for the first quantum ALU QUALU1 or a first nuclear electron microwave resonance frequency f _{MWCE1_1} for the first quantum ALU QUALU1. The quantum computer QC measures this first electron-nuclear radio wave resonance frequency f _{RWEC1_1} for the first quantum ALU QUALU1 and this first core-electron microwave resonance frequency (f _{MWCE1_1} ) for the first quantum ALU QUALU1, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The first quantum dot NV1 of the first quantum ALU QUALU1 can be used in the example 2 interact with a second core quantum point CI1 ₂ of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the first horizontal line LH1 and the first vertical line LV1 with a first horizontal current IH1 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a second electron nuclear radio wave resonance frequency f _{RWEC2_1} for the first quantum ALU QUALU1 or a second nuclear electron microwave resonance frequency f _{MWCE2_1} for the first quantum ALU QUALU1. The quantum computer QC measures this second electron-nuclear radio wave resonance frequency f _{RWEC2_1} for the first quantum ALU QUALU1 and this second core-electron microwave resonance frequency (f _{MWCE2_1} ) for the first quantum ALU QUALU1, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The first quantum dot NV1 of the first quantum ALU QUALU1 can be used in the example 2 interact with a third core quantum dot CI1 ₃ of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency genera tor MW/RF-AWFG, the first horizontal line LH1 and the first vertical line LV1 are energized with a first horizontal current IH1 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG has a third electron core -Radio wave resonance frequency f _{RWEC3_1} for the first quantum ALU QUALU1 or a third core-electron microwave resonance frequency f _{MWCE3_1} for the first quantum ALU QUALU1. The quantum computer QC measures this third electron-nuclear radio wave resonance frequency f _{RWEC3_1} for the first quantum ALU QUALU1 and this third core-electron microwave resonance frequency (f _{MWCE3_1} ) for the first quantum ALU QUALU1, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The second quantum dot NV2 of the second quantum ALU QUALU2 can be used in the example 2 interact with a first core quantum point CI2 ₁ of the second quantum ALU QUALU2 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the second horizontal line LH2 and the first vertical line LV1 with a second horizontal current IH2 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a fourth electron nuclear radio wave resonance frequency f _{RWEC1_2} for the second quantum ALU QUALU2 or a fourth nuclear electron microwave resonance frequency f _{MWCE1_2} for the second quantum ALU QUALU2. The quantum computer QC measures this fourth electron-nuclear radio wave resonance frequency f _{RWEC1_2} for the second quantum ALU QUALU2 and this fourth core-electron microwave resonance frequency (f _{MWCE1_2} ) for the second quantum ALU QUALU2, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The second quantum dot NV2 of the second quantum ALU QUALU2 can be used in the example 2 interact with a second core quantum point CI2 ₂ of the second quantum ALU QUALU2 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the second horizontal line LH2 and the first vertical line LV1 with a second horizontal current IH2 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a fifth electron nuclear radio wave resonance frequency f _{RWEC2_2} for the second quantum ALU QUALU2 or a fifth nuclear electron microwave resonance frequency f _{MWCE2_2} for the second quantum ALU QUALU2. The quantum computer QC measures this fifth electron-nuclear radio wave resonance frequency f _{RWEC2_2} for the second quantum ALU QUALU2 and this fifth core-electron microwave resonance frequency (f _{MWCE2_2} ) for the second quantum ALU QUALU2, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

The second quantum dot NV2 of the second quantum ALU QUALU2 can be used in the example 2 interact with a third core quantum point CI2 ₃ of the second quantum ALU QUALU2 when the microwave and/or radio wave frequency generator MW/RF-AWFG energizes the second horizontal line LH2 and the first vertical line LV1 with a second horizontal current IH2 and a first vertical current IV1, which the microwave and/or radio wave frequency generator MW/RF-AWFG modulates with a sixth electron nuclear radio wave resonance frequency f _{RWEC2_2} for the second quantum ALU QUALU2 or a sixth nuclear electron microwave resonance frequency f _{MWCE3_2} for the second quantum ALU QUALU2. The quantum computer QC measures this sixth electron-nuclear radio wave resonance frequency f _{RWEC3_2} for the second quantum ALU QUALU2 and this sixth core-electron microwave resonance frequency (f _{MWCE3_2} ) for the second quantum ALU QUALU2, preferably in an initialization step once by an OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory NVM, RAM of the computer core CPU of the control device µC, which it retrieves when the computer core CPU is to control the corresponding first core-electron quantum register CEQUREG1. The computer core CPU of the control device µC then sets the frequencies accordingly.

Since the coupling range of the quantum dots NV1, NV2 is greater, they can be coupled to one another. The second quantum dot NV2 of the second quantum ALU QUALU2 can be in the Example of the 2 interact with the first quantum dot NV1 of the first quantum ALU QUALU1 when the microwave and/or radio wave frequency generator MW/RF-AWFG supplies the first horizontal line LH1 and the second horizontal line LH2 and the first vertical line LV1 with a first horizontal current IH1 and a second horizontal current IH2 and a first vertical current IV1, which the microwave and / or radio wave frequency generator MW / RF-AWFG with an electron1-electron2 microwave resonance frequency f _MWEE12 for the coupling of the first quantum dot NV1 of the first quantum ALU QUALU1 with the second quantum dot NV2 modulated the second quantum ALU QUALU2. The computer core CPU of the quantum computer QC measures this electron1-electron2 microwave resonance frequency f _MWEE12 for the coupling of the first quantum dot NV1 of the first quantum ALU QUALU1, preferably once in the said initialization step by another OMDR measurement. The computer core CPU of the quantum computer QC stores the measured values in a memory RAM, NVM of the computer core CPU of the control device µC, which this computer core CPU retrieves when the corresponding electron-electron quantum register comprising the first quantum dot NV1 and the second quantum dot NV2 are controlled should. The computer core CPU of the control device µC then sets the frequencies accordingly.

Figure 3

3 shows the block diagram of an exemplary quantum computer QC with an exemplary, schematically indicated three-bit quantum register, which could possibly also be replaced, for example, by a three-bit core-electron-core-electron quantum register (CECEQUREG) with three quantum ALUs. An extension to an n-bit quantum register is easily possible for a person skilled in the art.

The core of the exemplary control device 3 is a control device μC which preferably includes a computer core CPU. The overall device preferably has a magnetic field control, preferably in the form of a first magnetic field control MFSx and a second magnetic field control MFSy and a third magnetic field control MFSz, which preferably receives its operating parameters from said control device µC and preferably returns operating status data to this control device µC. The magnetic field control MFSx, MFSy, MFSz is preferably a multi-dimensional controller whose task is to compensate for an external magnetic field through active counter-control. For this purpose, the magnetic field control MFSx, MFSy, MFSz preferably uses one or more magnetic field sensors MSx, MSy, MSZ, which preferably monitor the magnetic flux in the quantum computer QC, preferably in the vicinity of the quantum dots NV1, NV2, NV3 and those not shown in the figure for a better overview Core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ detected. The magnetic field sensors MSx, MSy, MSZ are preferably quantum sensors. Here is an example of the registrations DE 10 2018 127 394.0 , DE 10 2019 130 114.9 , DE 10 2019 120 076.8 and DE 10 2019 121 137.9 referred. With the help of the magnetic field control device, for example in the form of the first magnetic field generating means MGx and the second magnetic field generating means MGy and the third magnetic field generating means MGz and, the magnetic field control MFSx, MFSy, MFSz regulates the magnetic flux density B in the vicinity of the quantum dots NV1, NV2, NV3 and not in The core quantum points CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 1 , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ are drawn in _the figure for a better overview. The document presented here suggests that quantum sensors should preferably be used as magnetic field sensors MSx, MSy, MSZ, since these have the higher accuracy in order to sufficiently stabilize the magnetic field.

The control device µC preferably controls the horizontal and vertical driver stages HD1, HD2, HD3 via a control unit A CBA, which preferably energize the horizontal lines LH1, LH2, LH3 and vertical lines LV1 with the respective horizontal and vertical currents and the correct frequencies and timing Generate burst durations and burst positions based on a temporal starting point t ₀ .

The control unit A CBA sets the frequency and the pulse duration of the first horizontal shielding current ISH1 for the first horizontal shielding line SH1 in the first horizontal driver stage HD1 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the second horizontal shielding current ISH2 for the second horizontal shielding line SH2 in the first horizontal driver stage HD1 and in the second horizontal driver stage HD2 in accordance with the specifications of the control device µC.

The control unit A CBA sets the frequency and the pulse duration of the third horizontal shielding current ISH3 for the third horizontal shielding line SH3 in the second horizontal driver stage HD2 and in the third horizontal driver stage HD3 in accordance with the specifications of the control device µC.

The control unit A CBA sets the frequency in accordance with the specifications of the control device µC quency and the pulse duration of the fourth horizontal shielding current ISH4 for the fourth horizontal shielding line SH4 in the third horizontal driver stage HD3 and in the fourth horizontal driver stage HD4, which is only indicated due to lack of space.

The control unit A CBA sets the frequency and the pulse duration of the first horizontal current IH1 for the first horizontal line LH1 in the first horizontal driver stage HD1 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the second horizontal current IH2 for the second horizontal line LH2 in the second horizontal driver stage HD2 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the third horizontal current IH3 for the third horizontal line LH3 in the third horizontal driver stage HD3 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the first vertical shielding current ISV1 for the first vertical shielding line SV1 in the first vertical driver stage HV1 in accordance with the specifications of the control device μC.

The control unit A CBA sets the frequency and the pulse duration of the first vertical current IV1 for the first vertical line LV1 in the first vertical driver stage VD1 in accordance with the specifications of the control device μC.

Synchronized by the control unit A CBA, these driver stages VD1, HD1, HD2, HD3, HD4 feed their current into the lines SV1, LV1, SV2, SH1, LH1, SH2, LH2, SH3, LH3 in a fixed phase ratio based on a common synchronization time, SH4 on.

The following device elements of the proposed quantum computer QC are for electronic reading of the quantum states of the quantum dots NV1, NV2, NV3 or the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ necessary.

A control unit B CBB is connected to the control device µC via the control data bus SDB. The control device configures the control unit B CBB via the control data bus SDB and sets operating parameters and reads out data and operating states via the control data bus SDB. The control unit B CBB preferably detects the respective photocurrent that the receiver stages HS1, HS2, HS3, VS1 detect and makes the measurement data available to the control device µC via the control data bus SDB.

Previously, the control device µC configures a first horizontal receiver stage HS1 via the control data bus SDB and typically via the control unit B CBB in such a way that it takes the currents fed in by the first horizontal driver stage HD1 again on the other side of the lines.

The control device µC previously configures a second horizontal receiver stage HS2 via the control data bus SDB and typically via the control unit B CBB, preferably in such a way that it takes the currents fed in by the second horizontal driver stage HD2 again on the other side of the lines.

Previously, the control device µC configures a third horizontal receiver stage HS3 via the control data bus SDB and typically via the control unit B CBB in such a way that it takes the currents fed in by the third horizontal driver stage HD3 again on the other side of the lines.

Previously, the control device µC configures a first vertical receiver stage VS1 via the control data bus SDB and typically via the control unit B CBB in such a way that it takes the currents fed in by the first vertical driver stage VD1 on the other side of the lines.

Furthermore, the exemplary system of 3 a light source LD for pump radiation LB in the sense of this document. Using a light source driver LDRV, the control device µC can irradiate the quantum dots NV1, NV2, NV3 with the pump radiation LB via the optical system OS. When irradiated with this pump radiation LB, the paramagnetic centers of the quantum dots NV1, NV2, NV3 produce photoelectrons which pass through the first horizontal receiver stage HS1 and/or the second horizontal receiver stage HS2 and/or the third horizontal receiver stage HS3 and/or the first vertical receiver stage VS1 can be extracted by applying an extraction field, for example to the connected shielding lines SH1, SH2, SH3, SH4, SV1, SV2.

The microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms (English: arbitrary wave form generator) includes in the example the 3 the control unit A CBA, the first horizontal driver stage HD1, the second horizontal driver stage HD2, the third horizontal driver upper stage HD2 and the first vertical driver stage VD1.

In addition, the microwave and/or radio wave frequency generator MW/RF-AWFG for generating largely freely definable waveforms (Arbitrary Wave Form Generator) can also be understood in such a way that in the example of 3 the control unit B CBB, the first horizontal receiver stage HS1, the second horizontal receiver stage HS2, the third horizontal receiver stage HS2 and the first vertical receiver stage VS1.

The lines SV1, LV1, SV2, SH1, LH1, SH2, LH2, SH3, LH3, SH4 form the in the example 3 the exemplary microwave and/or radio wave antenna mWA.

Figure 4

4 shows an exemplary quantum computer system QUSYS with an exemplary central control unit ZSE. In this example, the exemplary central control unit ZSE is connected to a large number of quantum computers QC1 to QC16 via a preferably bidirectional data bus, the external data bus EXTDB. Such a quantum computer system QUSYS preferably includes more than one quantum computer QC1 to QC16. In the example of the 4 Each of the quantum computers QC1 to QC16 includes a control device µC1 to µC16. The quantum computer system QUSYS preferably comprises a charging device LDV, which charges an energy reserve BENG with the energy from a power supply PWR of the charging device LDV and/or supplies an energy processing device SRG with electrical energy. The energy processing device SRG supplies one or more device parts of the quantum computer system QUSYS with electrical energy from the energy reserve BENG and/or with electrical energy from the charging device LDV. The energy processing device SRG preferably supplies one or more device parts of the quantum computer system QUSYS with electrical energy from the energy reserve BENG when a device part of the quantum computer system QUSYS performs a quantum operation for manipulating a quantum dot NV1, NV2, NV3 and/or for manipulating a core quantum dot CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ executes. In the example of the 4 For example, 16 quantum computers QC1 to QC16 are connected to the central control device ZSE via the external data bus EXTDB. The external data bus EXTDB can be any suitable data transmission system. For example, it can be wired, wireless, fiber optic, optical, acoustic, radio-based. In the case of a wired system, the external data bus EXTDB can be, for example, a single-wire data bus, such as a LIN bus, or a two-wire data bus, such as a CAN data bus, in whole or in sections. The external data bus EXTDB can, for example, be a more complex data bus with several conductors and/or several logical levels, etc. in whole or in sections. The external data bus EXTDB can be an Ethernet data bus, for example, in whole or in parts. The external data bus EXTDB can consist entirely of one type of data bus or be composed of various data transmission routes of different types. The external data bus EXTDB can be star-shaped as in the example 4 be arranged. The external data bus EXTDB can be designed in whole or in part, for example as in a daisy chain (https://de.wikipedia.org/wiki/Daisy_Chain) as a chain of bus nodes in the form of the quantum computers QC1 to QC16, in which case each one is preferred the control devices of the quantum computers in question of this part of the quantum computer system QUSYS preferably have more than one data interface in order to be able to connect more than one external data bus EXTDB to the quantum computer in question, for example for such a chain. It is conceivable that one or more quantum computers QC1 to QC16 then act as bus masters and thus as central control devices ZSE for subordinate sub-networks of the QUSYS quantum computer system.

It is therefore also conceivable that the central control device ZSE of the quantum computer system QUSYS is the control device μC of a quantum computer QC or that the central control device ZSE of the quantum computer system QUSYS is a quantum computer QC a control device is µC, here in the case of 4 The emphasis is on the “normal” computer properties of the control device µC, which controls the quantum computer system QUSYS as the central control device ZSE. From the perspective of the quantum computers QC1 to QC16, the central control device ZSE corresponds to an external monitoring computer of the quantum computer system QUSYS.

The data transmission network of the quantum computer system QSYS can correspond entirely or in parts to a linear chain of bus nodes in the form of the quantum computers QC1 to QC16 along part of the external data bus EXTDB or along the external data bus EXTDB, which can also be closed to form a ring (keyword token ring). .

The data transmission network of the quantum computer system QSYS can be in whole or in part a star structure of bus nodes in the form of the quantum computers QC1 to QC16, which are connected to one or more data lines and/or data transmission media. A star structure is present, for example, when data is transmitted via radio. One, several or all of the quantum computers QC1 to QC16 can also be connected to the central control device ZSE via a point-to-point connection. In this case, the central control device ZSE must have a separate data interface for each point-to-point connection.

The data transmission network of the quantum computer system QSYS can be designed as a tree structure, whereby individual quantum computers, for example, have more than one data bus interface and can serve as a bus master, i.e. central control device ZSE for the sub-network of the data transmission network made up of data buses and quantum computers.

The quantum computer system QUSYS can thus be structured hierarchically, with the control devices μC of individual quantum computers being the central control device ZSE of sub-quantum computer systems. The sub-quantum computer systems are themselves QUSYS quantum computer systems. The central control device ZSE of the sub-quantum computer system is preferably itself a quantum computer, which itself is preferably part of a higher-level quantum computer system QUSYS.

This hierarchy allows different calculations to be processed in parallel in different sub-quantum computer systems, with the number of quantum computers used being chosen differently depending on the task.

The quantum computer system QUSYS therefore preferably comprises several computer units coupled to one another. The computer units are typically computer cores CPU of the control devices µC of the quantum computers QC1 to QC16. Such a computing unit can use an artificial intelligence program that can be coupled to the quantum computers and/or the quantum registers and/or the quantum bits. Both the input into the artificial intelligence program can depend on the state of the quantum dots of these components of the quantum computer system, and the control of the quantum bits and quantum dots of these components of the quantum computer system can depend on the results of the artificial intelligence program. The artificial intelligence program can be executed both in the central control device ZSE and in the control devices µC1 to µC16 of the quantum computers QC1 to QC16. Here, only parts of the artificial intelligence program in which the central control device ZSE can be executed, while other parts of the artificial intelligence program can be executed in the control devices µC of quantum computers within the quantum computer system. Also, only parts of the artificial intelligence program can be executed in one of the control devices µC1 to µC16 of the quantum computers QC1 to QC16, while other parts of the artificial intelligence program are executed in other control devices µC1 to µC16 of other quantum computers QC1 to QC16 within the quantum computer system QUSYS become. This processing of an artificial intelligence program can therefore be distributed over the quantum computer system QUSYS or can be concentrated in a control device of the control devices µC1 to µC16 of the quantum computers QC1 to QC16. The artificial intelligence program works together with quantum points NV1, NV2, NV3 of the quantum computers QC1 to QC16. The control device can actually also be a system of control devices µC1 to µC16. A control device can include, for example, the central control device ZSE of a quantum computer system QSYS with one or more quantum dots NV1, NV2, NV3 and / or one or more control devices µC of one or more quantum computers QC1 to QC16, each with one or more quantum dots NV1, NV2, NV3 . More complex topologies with additional intermediate computer nodes and data bus branches are conceivable. The control device, which as described can also be a combination of control devices, executes an artificial intelligence program. Such an artificial intelligence program can be, for example, a neural network model with neural network nodes.

For example, one or more of the control devices of the control devices µC1 to µC16, the quantum computers QC1 to QC16 and/or the central control unit ZSE can execute a machine learning method. The paper presented here refers, for example, to Akinori Tanaka, Akio Tomiya, Koji Hashimoto, “Deep Learning and Physics (Mathematical Physics Studies)” February 21, 2021, publisher: Springer; 1st ed. 2021 Edition, ISBN-10: 9813361077, ISBN-13: 978-9813361072 and Ovidiu Calin, “Deep Learning Architectures: A Mathematical Approach (Springer Series in the Data Sciences),” Springer; 1st ed. 2020 Edition (February 14, 2021), ISBN-10: 3030367231, ISBN-13: 978-3030367237. The procedures explained in these documents are part of the Disclosure of the document presented here, provided that a quantum computer carries out QC as described in the document presented here. One of the most common techniques in artificial intelligence that a proposed quantum computer QC and/or a proposed quantum computer system QUSYS can perform is machine learning. Machine learning is a self-adaptive algorithm that a proposed quantum computer QC and/or a proposed quantum computer system QUSYS can execute. The so-called deep learning that a proposed quantum computer QC and/or a proposed quantum computer system QUSYS can execute is typically a subset of machine learning. A proposed quantum computer QC and/or a proposed quantum computer system QUSYS use a series of hierarchical layers or a hierarchy of concepts in machine learning to carry out the machine learning process. The proposed quantum computer QC or the proposed quantum computer system QUSYS preferably use a model of artificial neural networks that are virtually organized and constructed like the human brain. The virtual neurons of the neural network model, which the proposed quantum computer QC or the proposed quantum computer system QUSYS executes, are preferably virtually connected to one another like a network. The first virtual layer of the neural network, the visible input layer, processes raw data input, such as the individual pixels of an image. Data input contains variables accessible to observation, hence “visible layer”. This first virtual layer of the neural network model forwards its outputs to the next virtual layer of the network model when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. This second virtual layer processes the information from the previous virtual layer and also passes on the result when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. The next third virtual layer of the neural network model receives the information of the second virtual layer when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. The third virtual layer of the neural network model further processes this information when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. These layers are called hidden layers. The features they contain are becoming increasingly abstract. Their values are not specified in the original data. Instead, when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS, the neural network model should preferably determine which concepts are useful for explaining the relationships in the observed data. This now continues across all virtual levels of the artificial neural network model. The result is output in the visible last virtual layer when the neural network model is executed by the proposed quantum computer QC or by the proposed quantum computer system QUSYS. This breaks down the desired complicated data processing into a series of nested simple mappings, each describing a different layer of the neural network model.

The neural network model typically uses one or more input values and/or one or more input signals. The neural network model typically provides one or more output values and/or one or more output signals. It is now proposed here to supplement the artificial intelligence program with a program that carries out one or more of the above-mentioned quantum operations on one or more quantum computers of the quantum computers QC1 to QC16. This coupling CAN, FOR EXAMPLE, happen in one direction by driving one or more quantum dots QC1 to QC16. in particular by means of horizontal lines LH1, LH2, LH3 and/or vertical lines LV1, depends on one or more output values and/or one or more output signals of the neural network model. In the other direction, states of one or more quantum dots are read out at a time and used as input in the artificial intelligence program, in this example the neural network model. The value of one or more input values and/or one or more input signals of the artificial intelligence program, here the neural network model, then depends on the state of one or more of the quantum dots NV1, NV2, NV3 and/or one or more core quantum dots _CI11 , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ from.

Figure 5

5 shows an aircraft FZ with several deployable quantum computers QC1, QC2. By Example of the 5 the exemplary aircraft FZ has a first quantum computer QC1 and a second quantum computer QC2 and a central control unit ZSE, which is connected to the exemplary two quantum computers QC1, QC2 via an external data bus EXTDB. The external data bus EXTDB is the preferred part of the proposed aircraft FZ. The deployable quantum computers QC1, QC2 preferentially solve NP-hard problems in the proposed aircraft FZ.

• • https://de.wikipedia.org/wiki/NP_(Komplexit%C3%A4tsklasse) und
• • https://en.wikipedia.org/wiki/NP-hardness

For more information on NP-hard problems, see for example

• • https://de.wikipedia.org/wiki/NP_(Komplexit%C3%A4tsklasse) and
• • https://en.wikipedia.org/wiki/NP-hardness

Such problems can, for example, concern the arrangement of certain loads in the cargo hold or optimization problems such as the optimal travel route. It is also conceivable that the deployable quantum computers QC1, QC2 in the aircraft FZ carry out or support artificial intelligence tasks. The deployable quantum computers QC1, QC2 are preferably connected via the external data bus EXTDB to the central control device ZSE, which is typically another control device of the aircraft FZ. For example, the central control device ZSE can be a computer system in the cockpit of the aircraft FZ or in a server room of the aircraft FZ. The proposed aircraft FZ thus preferably comprises a quantum computer system QUSYS with at least one quantum computer QC1, QC2.

The quantum computers QC1, QC2 can also support the pilots and the other computer systems of the FZ aircraft. For example, the quantum computers QC1, QC2 of the aircraft FZ can support the flight attitude control system FLR and/or the navigation system and the autopilot NAV or can take over their function in whole or in part. Of course, the functions of a quantum computer QC are not limited to these functions of an aircraft FZ.

For example, the following come into question:

Airborne Weather Radar

The evaluation of the Airborne Weather Radar: The weather radar is usually installed in the nose behind a radome, a closed protective cover (radar nose), of the FZ aircraft. It determines the weather in the area. The weather radar can transmit data to one or more quantum computers QC1, QC2 via the external data bus EXTDB. The quantum computers QC1, QC2 can then evaluate the data from the weather radar. The quantum computers QC1, QC2 preferably receive further data, for example via radio interfaces of the aircraft FZ, from other places, such as weather services, airline headquarters, aircraft manufacturers, etc. Typical NP complete problems that can be solved particularly well with quantum computers QC in this context are the evaluation of Weather data and the optimization of the flight route in terms of danger, flight time, costs, etc. The quantum computers QC1, QC2 can carry out these calculations of NP-complete problems and warn the pilots of dangerous weather phenomena at an early stage and make suggestions for optimization. If necessary, the aircraft's conventional computer systems can once again verify the results of the quantum computer programs that were executed on the quantum computers QC1, QC2 in a conventional manner, since then no optimization search is necessary, and confirm to the pilots the correctness of the quantum computer calculation. The document presented here refers to this as an example 9 .

ECAM (Electronic Centralized Aircraft Monitoring) or EICAS (Engine Indication and Crew Alerting System)

Another possible application is, for example, support for the ECAM (Electronic Centralized Aircraft Monitoring) by the quantum computers QC1, QC2 of the aircraft's quantum computer system QUSYS. This electronic system preferably displays the most important engine parameters in the aircraft and checks all aircraft systems, such as fuel and hydraulics. It reports errors and provides information on how to resolve the problem. This electronic system typically displays the most important engine parameters in the FZ aircraft and checks all aircraft systems, such as fuel and hydraulics. It reports suspected or detected errors and provides information on how to resolve the problem. For this purpose, the quantum computers QC1, QC2 can carry out quantum computer calculations in order to be able to recognize the probabilities of critical combinations of aircraft and environmental parameters and to determine measures, sequences of measures and flight routes, etc. in such a way that the probability of critical situations is minimized with maximum effectiveness.

TCAS (Traffic Alert and Collision Avoidance System)

The TCAS is an on-board early warning system of the proposed aircraft FZ to avoid aircraft collisions in the air. If two aircraft are on a collision course, it recommends this both pilots take a suitable evasive maneuver to avert an impending collision. The quantum computers QC1, QC2 can, for example, taking into account the weather conditions, etc., suggest alternative courses that, firstly, have a minimal probability of collision and, secondly, are also optimal with regard to the weather conditions.

Figure 6

Figure 6a

6a shows another example of the use of the proposed deployable quantum computer QC in an aircraft FZ. In the example of the 6a it is a military aircraft FZ. A military aircraft may, for example, be an interceptor, a long-range bomber, or a general combat aircraft, or a helicopter, or the like.

It could also be a drone or something similar.

In the example of the 6a The fighter aircraft includes a quantum computer QC. The quantum computer QC can, for example, in cooperation with a central control unit ZSE of the aircraft FZ, solve the NP-complete problem of risk assessment of objects in the area around the aircraft and along the route to the target, target selection and target definition and the sequence of target engagement, ammunition and weapon selection and work on the fastest and at the same time least risky route to the destination. The quantum computer QC is in the example 6 connected to the central control unit ZSE via an external data bus EXTDB within the aircraft FZ. The quantum computer QC preferably corresponds to a quantum computer QC 1 or the previous description.

In the example of the 6a The exemplary fighter aircraft FZ is armed with a first missile RKT and a second missile RKT. Instead of arming with RKT rockets and/or in addition to arming with rockets, arming with other weapons such as automatic cannons, jammers, reconnaissance devices, etc. is also conceivable. In this respect, the rockets are just examples of additional equipment that can be transported as payload by the FZ fighter aircraft. In this respect, the FZ aircraft is just an example of a vehicle in the broadest sense.

In the example of the 6a The vehicle in the form of the aircraft FZ has a quantum computer system similar to QUSYS 4 with one or more central control devices ZSE, which are connected to one or more quantum computers QC via one or more external data buses EXTDB.

In the example of the 6a The payload in the exemplary form of two RKT rockets each has its own quantum computer systems similar to QUSYS 4 with one or more central control devices ZSE of the respective payload, which are connected via one or more external data buses EXTDB of the respective payload to one or more quantum computers QC of the respective payload. In the example of the 6a Each of the two exemplary rockets RKT has its own quantum computer system QUSYS of the respective rocket RKT similar to 4 with one or more respective central control devices ZSE of the respective rocket RKT, which are connected to one or more quantum computers QC of the respective rocket RKT via one or more external data buses EXTDB of the respective rocket RKT.

In the state shown, the FZ fighter aircraft therefore has several QUSYS quantum computer systems. A first quantum computer system QUSYS includes at least one central control unit ZSE of the fighter aircraft FZ and at least one external data bus EXTDB of the fighter aircraft FZ and at least one quantum computer QC of the fighter aircraft FZ. An exemplary second quantum computer system QUSYS includes at least one central control unit ZSE of the first exemplary rocket RKT and at least one external data bus EXTDB of the first exemplary rocket RKT and at least one quantum computer QC of the first exemplary rocket RKT. An exemplary third quantum computer system QUSYS includes at least one central control unit ZSE of the second exemplary rocket RKT and at least one external data bus EXTDB of the second exemplary rocket RKT and at least one quantum computer QC of the second exemplary rocket RKT.

The document presented here proposes that an external data bus EXTDB connects the first quantum computer system to the second and third quantum computer systems as long as the payloads are connected to the aircraft FZ.

After the rockets RKT have been fired, i.e. when the aircraft FZ separates from its payload in the form of the rockets RKT, a quantum computer system separation device QCTV separates the quantum computer system QUSYS of the separated payload, here the fired rocket RKT, from the quantum computer system QUSYS of the aircraft FZ. The vehicle here is, for example, an airplane FZ. A vehicle in the sense of the document presented here can also be a motor vehicle, a two-wheeler, a tricycle or a truck, a commercial vehicle, a robot, a transport vehicle, a drone, a robot drone, a missile, a floating body, a submersible body , a ship, a submarine, a sea mine, a landmine, a rocket, a projectile, a satellite, a space station, a trailer, a barge, a container, in particular a sea container or the like. The quantum computer system separation device QCTV preferably separates an external data bus EXTDB, which, for example, connects a first quantum computer system QUSYS with a second quantum computer system QUSYS, if necessary, so that the quantum computer system QUSYS, which previously included the first and the second quantum computer system QUSYS, is separated by the separation using the quantum computer system separation device QCTV in two separate quantum computer systems QUSYS disintegrates. The quantum computer system separating device QCTV can also conversely connect a previously separate first quantum computer system QUSYS with a previously separate second quantum computer system QUSYS, for example via one or more external data buses EXTDB and, if necessary, couple them, so that a new, enlarged quantum computer system QUSYS is created, which then the first and the second Quantum computer system QUSYS comprises merging into a quantum computer system QUSYS by connecting these two quantum computer systems via quantum computer system separation device. In such a new quantum computer system QUSYS made up of at least two previously separate quantum computer systems QUSYS, the central control unit ZSE of the quantum computer system QUSYS of the vehicle, here the fighter aircraft FZ, is preferably given higher priority than the central control unit ZSE of the quantum computer system QUSYS of the payload, here the rocket RKT. This merger is particularly advantageous during the loading process when the payload is connected to the vehicle.

After the payload has been separated from the vehicle, the quantum computer system QUSYS can preferably act autonomously. In the example of the 6a This means that after the separation of the missiles RKT as an exemplary payload from the fighter aircraft FZ as an exemplary vehicle, the quantum computer system QUSYS of the missile RKT can preferably act autonomously. However, it is conceivable that the quantum computer system QUSYS of the payload, here in the form of a rocket RKT, after separation from the vehicle, here in the form of the fighter aircraft FZ, via a wireless or wired or via an optical fiber or a functionally equivalent data transmission link with the quantum computer system QUSYS of the vehicle, here the FZ fighter aircraft, remains connected. In an extreme case, it is conceivable that, for example, each of the quantum computers QC1 to QC16 4 is the quantum computer QC of an individual vehicle, which is connected to a central control unit ZSE in a lead vehicle and/or to each other via a radio link as an external data bus EXTDB. For example, an exemplary quantum computer system QUSYS can be a swarm of drones, in which each of the drones includes one or more quantum computers QC that communicate with each other wirelessly, for example via radio links or laser beam connections as an external data bus EXTDB. In the exemplary case of a swarm of drones, the quantum computer system QUSYS of the quantum computers QC1 to QC16 of the exemplary drones cannot include a central control device ZSE. All drones are preferably designed in approximately the same way and then preferably organize themselves using swarm technologies.

In the example of the 6a For example, each rocket RKT includes a quantum computer QC. The quantum computer QC can, for example, in cooperation with a central control unit ZSE of the relevant missile RKT, solve the NP-complex problem of risk assessment of objects in the vicinity of the relevant missile RKT and along the route of the relevant missile RKT to the target, the target selection and target definition and the sequence of the Target combat by selecting ammunition and weapons and working on the fastest and least risky route to the target. The RKT missile can also be a drone or a cruise missile that can engage multiple targets if necessary. The quantum computer QC of the rocket in question is RKT in the example 6a connected via an external data bus EXTDB within the relevant rocket RKT to the central control unit ZSE of the relevant rocket RKT. The quantum computer QC of the relevant rocket RKT preferably corresponds to a quantum computer QC 1 or the previous description.

Figure 6b

The 6b shows an exemplary deployable quantum computer QC in a sea container SC on a low-loader TL with a tractor ZM. Both the sea container SC and the low-loader TL as well as the tractor ZM can include one or more quantum computers QC and/or one or more quantum computer systems QUSYS. One or more quantum computers QC and/or one or more quantum computer systems can be installed within the sea container SC teme QUSYS must be placed. All of these quantum computers QC and/or quantum computer systems QUSYS can be transferred to one or more quantum computer systems QUSYS during transport and/or before and/or afterwards, as in the example 6a explained in particular be interconnected at times. In the example of the 6c An additional energy reserve BENG supplies the quantum computer system QUSYS with the quantum computer QC within the exemplary sea container SC with electrical energy.

Figure 6c

The 6c shows an exemplary aircraft carrier FZT. The exemplary aircraft carrier FZT includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. The exemplary aircraft carrier FZT is an example of a warship that includes one or more QC quantum computers and/or one or more QUSYS quantum computer systems. The exemplary aircraft carrier FZT is an example of a ship that includes one or more QC quantum computers and/or one or more QUSYS quantum computer systems. The exemplary aircraft carrier FZT is an example of a floating body that includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. The exemplary aircraft carrier FZT is an example of a vehicle that includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. The quantum computers QC and/or quantum computer systems QUSYS are preferably deployable quantum computers QC in the sense of the document presented here. For example, quantum computer systems QUSYS and / or quantum computers QC of aircraft FZ of the aircraft carrier FZT during transport through the aircraft carrier FZT and / or in the aircraft carrier FZT with one or more quantum computers QC and / or quantum computer systems QUSYS of the aircraft carrier FZT, for example via one or more quantum computer system separation devices QCTV and one or more external data buses EXTDB connected to larger quantum computer systems QUSYS.

In the example of the 6c For example, the aircraft carrier FZT includes one or more quantum computers QC and/or one or more quantum computer systems QUSYS. One or more of these quantum computers QC and / or one or more quantum computer systems QUSYS can, for example, in cooperation with a central control unit ZSE of the aircraft carrier FZT, solve the NP-complete problem of risk assessment of objects in the environment of the aircraft carrier FZT and along the route to a target, the target selection and target definition and the sequence of attacking the target, the selection of aircraft, ammunition and weapons and the fastest and at the same time lowest-risk route to the target. The quantum computer(s) QC and/or the quantum computer system(s) QUSYS of the aircraft carrier FZT are preferably connected to each other and to those of other devices on the aircraft carrier FZT via an external data bus EXTDB and, if necessary, suitable quantum computer system separation devices QCTV within the aircraft carrier FZT. A quantum computer QC from the aircraft carrier FZT preferably corresponds to a quantum computer QC from the 1 or the previous description.

Figure 6d

The 6d shows a factory hall FHB as an example of a stationary device into which several QC quantum computers were installed. In the example of the 6d The normal power network PWR supplies the deployable quantum computer systems QUSYS with their quantum computers QC within the exemplary stationary devices FBH with electrical energy. The stationary device FHB can, for example, comprise one or more quantum computer systems QUSYS with one or more quantum computers QC. The quantum computer(s) QC and/or the quantum computer system(s) QUSYS of the stationary device FHB are preferably connected to each other and to those of other devices of the stationary device FHB via an external data bus EXTDB and, if necessary, suitable quantum computer system separation devices QCTV within the stationary device FHB. A quantum computer QC of the stationary device FHB preferably corresponds to a quantum computer QC of 1 or the previous description.

Figure 7

7 shows another example of a vehicle with a proposed quantum computer system QUSYS, here with two quantum computers QC as an example. It is an exemplary submarine SUB. The exemplary submarine SUB has an energy system ERS as the energy source of the submarine SUB. The energy system ERS also represents the energy supply PWR of the charging device LDV of the quantum computer system QUSYS of the submarine SUB. The submarine SUB typically has a very large energy reserve BTR. A drive ENG drives in the example 7 the submarine SUB via one or more exemplary ship screws SCHR.

In the example of the 7 The submarine SUB has a number of RKT missiles as armament. They can also be cruise missiles or other devices that are located on the submarine SUB as devices that can be separated from the submarine SUB. In this respect, the RKT rockets are only examples of devices that can be separated from a vehicle and, for example, as a payload here, are located on or in the vehicle, here a submarine SUB. For example, one or more of the missiles RKT of the submarine SUB may include one or more quantum computer systems QUSYS and/or one or more quantum computers QC. Preferably, the one or more quantum computer systems QUSYS and/or one or more quantum computers QC are connected to the one or more quantum computer systems QUSYS and/or the one or more quantum computers QC1, QC2 of the submarine SUB by means of a quantum computer system separation device QCTV and an external data bus EXTDB tied together. The document presented here already describes the separation and connection of quantum computer systems QUSYS in the description 6a . Here the submarine SUB takes on the role of the aircraft FZ 6a a. The relationships disclosed there also apply here where applicable and are used where appropriate and sensible. A missile launch control RKTC is an example of a vehicle fire control system. Here the vehicle is the submarine SUB. In the example of the 7 The missile launch control RKTC and the submarine SUB can each have one or more quantum computer systems QUSYS and / or one or more quantum computers QC. Since the missile launch control RKTC is part of the submarine, the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the missile launch control RKTC are also part of the submarine SUB. An external data bus EXTDB preferably connects the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the missile launch control RKTC with the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the submarine SUB.

In the example of the 7 The submarine SUB has a number of TRP torpedoes as armament. They can be cruise missiles or other devices that are located on the submarine SUB as devices that can be separated from the submarine SUB and are separated, for example, via the torpedo tubes as an example of a mechanical separation device, for example by firing. In this respect, the TRP torpedoes are only examples of devices that can be separated from a vehicle and, for example, as a payload here, are located on or in the vehicle, here a submarine SUB. For example, one or more of the torpedoes TRP of the submarine SUB may include one or more quantum computer systems QUSYS and/or one or more quantum computers QC. The one or more quantum computer systems QUSYS and/or one or more quantum computers QC are preferred by means of a quantum computer system separation device QCTV and an external data bus EXTDB with the one and/or more quantum computer systems QUSYS and/or the one or more quantum computers QC1, QC2 of the submarine SUB tied together. The document presented here already describes the separation and connection of quantum computer systems QUSYS in the description 6a . Here the submarine SUB takes on the role of the aircraft FZ 6a a. The connections disclosed there also apply here where applicable and are used where appropriate and meaningful. A torpedo launch control TRPC is an example of a vehicle's fire control system. Here the vehicle is the submarine SUB. In the example of the 7 The torpedo launch control TRPC and the submarine SUB can each have one or more quantum computer systems QUSYS and / or one or more quantum computers QC. Since the torpedo launch control TRPC is part of the submarine SUB, the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the torpedo launch control RKTC are also part of the submarine SUB. An external data bus EXTDB preferably connects the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the torpedo launch control TRPC with the one or more quantum computer systems QUSYS and / or the one or more quantum computers QC of the submarine SUB.

In addition, the submarine SUB in the example has the 7 preferably via a large number of sensors SENS, which, for example, connects an external data bus EXTDB with one or more quantum computer systems QUSYS and / or quantum computers QC on board the submarine SUB. These can be, for example, sound sensors and/or ultrasonic sensors, conductivity sensors, antennas, sensors for electromagnetic and/or ionizing radiation, particle detectors, pressure sensors, speed sensors, position sensors, attitude sensors, acceleration sensors, magnetometers, LIDAR sensors, RADAR sensors, quantum sensors and the like act equally. The SENS sensors can also be sensors systems, sensor arrays and other measurement systems. The SENS sensors can record measured values inside and outside the vehicle, here a submarine SUB.

In the example of the 7 For example, one or more quantum computers QC and / or one or more quantum computer systems QUSYS on board the vehicle, here a submarine SUB, for example in cooperation with a central control unit ZSE of the vehicle, the NP-complete problem of risk assessment of objects in the area around the vehicle, here for example the submarine SUB, and/or along the course to the target of the vehicle, the target selection and target definition and the sequence of target engagement, the ammunition and weapon selection and the fastest and at the same time lowest-risk route of the vehicle to the target. The quantum computers QC1, QC2 of the submarine SUB and the other device parts are in the example 7 connected to the central control unit ZSE of the submarine SUB via an external data bus EXTDB within the submarine SUB. The quantum computers QC1, QC2 and those of the other device parts preferably correspond to a quantum computer QC 1 or the previous description.

Figure 8

8th shows an exemplary vehicle with a first quantum computer QC1, a second quantum computer QC2, a central control unit ZSE and an external data bus EXTDB, which connects them to a quantum computer system QUSYS. The vehicle in the example is the 8th an exemplary motor vehicle. As exemplary sensors SENS, the vehicle includes a GPS receiver GPS for determining the current position on the earth's surface and a navigation system NAV. The vehicle may include one or more quantum computers QC and/or one or more quantum computer systems QUSYS, which may be interconnected via one or more external data buses EXTDB. The one or more external data buses can connect the one or more quantum computers QC and/or one or more quantum computer systems QUSYS with one or more actuators and/or one or more sensors. The sensors can also be sensor systems. For example, these can be acceleration and position sensors, impact sensors, ultrasonic measurement systems, radar systems, LIDAR systems, drive sensor systems and energy storage systems, etc. The actuators can be transmitters, lasers, motors, etc.

In the example of the 8th For example, one or more quantum computers QC and / or one or more quantum computer systems QUSYS on board the vehicle, here a car, for example in cooperation with a central control unit ZSE of the vehicle, the NP-complete problem of risk assessment of objects in the area around the vehicle, here for example the car, and/or along the route to the vehicle's destination, the destination selection and destination definition and the order of approach to the destination and the fastest and at the same time lowest-risk route of the vehicle to the destination. The quantum computers QC1, QC2 of the vehicle, here an example of the car, and the other device parts of the vehicle, here an example of the car, are in the example 8th via an external data bus EXTDB within the vehicle, here for example the car, preferably connected to the central control unit ZSE of the vehicle, here for example the car. The quantum computers QC1, QC2 and those of the other device parts preferably correspond to a quantum computer QC 1 or the previous description.

Figure 9

9 shows a typical solution to an NP-complete problem. The development of the proposal presented here showed that problem solving with a quantum computer takes place in four instead of three steps.

Computer programs that run on conventional computers with Harvard or non-Neumann architecture prefer to solve problems using the steps of analysis, elaboration and synthesis.

In the analysis step (step A)), the computer adapts the problem to the way the computer works. For example, a read routine translates a text file with readable numbers into binary data that is stored in the computer's memory.

In a second step, elaboration (step B), the computer then carries out a calculation in which, for example, these binary data serve as input data and determines binary result data.

In a third step, the synthesis step (step D), the computer adapts this result to the intended use. For example, in the example described here, the computer could convert the binary result data into readable digits of the corresponding numbers in an output text file.

The elaboration has now shown that, particularly in safety-relevant applications, after a solution to an NP-complete problem in elaboration step B) using a quantum computer QC, the quantum computer system QUSYS must carry out a check in step C). In this test step, the quantum computer system QUSYS or the quantum computer QC checked, preferably using a conventional computer core CPU or a central control unit ZSE, whether the solution determined in the elaboration is actually a solution. Quantum operations are always statistical operations that can also produce incorrect results. If necessary, the QUSYS quantum computer system repeats the calculation.

Figure 10

10 equals to 4 , whereby the 16 quantum computers QC1 to QC16 of the quantum computer system QUSYS are now inserted into the external data bus EXTDB as an example. The control device μC, for example, of each of the quantum computers QC1 to QC16, has, for example, two external data interfaces DBIFa and DBIFb instead of a data bus interface DBIF, as in 1 shown. This allows, for example, the central control unit ZSE to assign each of the quantum computers QC a unique bus node address. Typically, the control devices µC of the quantum computers QC1 to QC16 pass on data that they pass on from the data bus side with the central control device ZSE to quantum computers and bus nodes on the other half of the data bus only if they themselves have already received a valid bus node address from the central control device ZSE. In this way, the central control device ZSE can gradually assign a quantum computer address as a bus node address of the external data bus EXTDB to all quantum computers of the quantum computers QC1 to QC16, starting with the first quantum computer QC1. After switching on or a system reset, all quantum computers QC1 to QC16 preferably have an invalid default quantum computer address that is typically the same as the initial bus node address. As a result, the central control device can provide the quantum computer QC1 to QC16 that is not yet provided with a valid bus node address and is closest to it with a valid bus node address. As a result, in the next step, the central control device ZSE can reach and initialize the underlying quantum computer of the quantum computers QC1 to QC16 and so on until all quantum computers of the quantum computers QC1 to QC16 have received a valid quantum computer address as a bus node address. After switching on, the quantum computer system QSYS preferably carries out an initialization of the quantum computers QC1 to QC16 of the quantum computer system QUSYS. The initialization of the QUSYS quantum computer system preferably also includes carrying out an auto-addressing process for assigning bus node addresses to the bus nodes of the external data bus EXTDB. In the example of the 10 The bus nodes are the quantum computers QC1 to QC16. In the example of the 10 The central control device ZSE preferably takes on the role of a bus master, which generates and assigns the bus node addresses and controls the quantum computers QC1 to QC16.

Figure 11

11 shows an exemplary quantum computer system QUSYS with four sub-quantum computer systems.

The first quantum computer QC1 forms a first sub-quantum computer system with the second quantum computer QC2 and the third quantum computer QC3 and the fourth quantum computer QC4. A first sub-data bus UDB1 connects the quantum computers QC1, QC2, QC3, QC4 of the first sub-quantum computer system. The first quantum computer QC1 can serve as a bus master for the other quantum computers QC2, QC3, QC4 of the first sub-quantum computer system.

The fifth quantum computer QC5 forms a second sub-quantum computer system with the sixth quantum computer QC6 and the seventh quantum computer QC7 and the eighth quantum computer QC8. A second sub-data bus UDB2 connects the quantum computers QC5, QC6, QC7, QC8 of the second sub-quantum computer system. The fifth quantum computer QC5 can serve as a bus master for the other quantum computers QC6, QC7, QC8 of the second sub-quantum computer system.

The ninth quantum computer QC9 forms a third sub-quantum computer system with the tenth quantum computer QC10 and the eleventh quantum computer QC11 and the twelfth quantum computer QC12. A third sub-data bus UDB3 connects the quantum computers QC9, QC10, QC11, QC12 of the third sub-quantum computer system. The ninth quantum computer QC9 can serve as a bus master for the other quantum computers QC10, QC11, QC12 of the third sub-quantum computer system.

The thirteenth quantum computer QC13 forms a four with the fourteenth quantum computer QC14 and the fifteenth quantum computer QC15 and the sixteenth quantum computer QC16 th sub-quantum computer system. A fourth sub-data bus UDB4 connects the quantum computers QC13, QC14, QC15, QC16 of the fourth sub-quantum computer system. The thirteenth quantum computer QC13 can serve as a bus master for the other quantum computers QC14, QC15, QC16 of the fourth sub-quantum computer system.

In the example of the 11 The external data bus EXTDB connects the first quantum computer QC1 and the fifth quantum computer QC5 and the ninth quantum computer QC9 and the thirteenth quantum computer QC13 and the central control unit ZSE.

Figure 12

12 shows the solution of an NP-complete problem using a mobile deployable quantum computer QC. Such a method begins with the acquisition of environmental data by the QUSYS quantum computer system in step A). The environmental data is typically collected using suitable sensors, which can be part of the quantum computer system QUSYS or which are connected to this quantum computer system QUSYS via data connections and transmit environmental data to the quantum computer system QUSYS. In a step B), the quantum computer system QUSYS identifies objects in the environment of the quantum computer system QUSYS, whereby this environment can also be distant from the quantum computer system QUSYS. In step C), the quantum computer system QUSYS classifies the identified objects in the environment of the quantum computer system QUSYS. Typically, in step C), the quantum computer system QUSYS classifies the objects according to danger and/or vulnerability and/or strategic effect in order to maximize a weapon effect. This classification is preferably carried out in step C) using a neural network model, which the quantum computer system QUSYS preferably executes. For this step C), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out the classification of the objects. In a step D, the quantum computer system QUSYS determines the weapons and/or the ammunition and/or the configuration and/or the order of the attacked objects and/or the attacked and/or the non-attacked objects. This determination is preferably carried out in step D) using a neural network model, which the quantum computer system QUSYS preferably executes. In step D), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out these determinations. In a step E), the quantum computer system QUSYS preferably suggests one or more of these specified attack scenarios to an operator, for example one or more pilots and/or several fire control officers or the like. If they give the order to fire, the quantum computer system QUSYS, for example, can implement the released attack scenario in a step F).

This example application can be generalized to solve NP-complete problems. Such a generalized method begins with the acquisition of data by the quantum computer system QUSYS in a step A). The data is typically collected using suitable sensors and/or databases or other data sources, which can be part of the quantum computer system QUSYS or which are connected to this quantum computer system QUSYS via data connections and transmit the data to the quantum computer system QUSYS. In a step B), the quantum computer system QUSYS identifies suitable data objects. In step C), the QUSYS quantum computer system classifies the identified data objects. Typically, in step C), the quantum computer system QUSYS classifies the objects according to categories that are relevant to solving the respective problem in order to maximize the effect. This classification is preferably carried out in step C) using a neural network model, which the quantum computer system QUSYS preferably executes. For this step C), the quantum computer system QUSYS preferably uses one or more quantum operations to manipulate the quantum state of one or more quantum points NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the quantum computer system QUSYS in order to carry out the classification of the data objects. In a step D), the quantum computer system QUSYS determines the means for achieving the purpose and the parameters and means configurations when using these means and/or the order of the processed or unprocessed data objects and/or the order of the means used. This determination is preferably carried out in step D) using a neural network model, which the quantum computer system QUSYS preferably executes. The quantum computer system QUSYS preferably uses one or more quantum operations in step D) to manipulate the quantum state of one or more quantum dots NV1, NV2, NV3 of one or more quantum computers QC1 to QC16 of the Quantencom computer system QUSYS to carry out these specifications. In a step E), the quantum computer system QUSYS preferably suggests one or more of these specified scenarios to an operator or the like. If they give a start signal, the QUSYS quantum computer system can, for example, implement the released scenario in a step F).

Figure 13

The 13 shows an exemplary structure of an amplifier V, as shown in the 1 is marked. An internal amplifier IVV of the amplifier V amplifies and filters the receiver output signal S0 to an output signal V1 of the internal amplifier IVV of the amplifier V. An analog-to-digital converter ADCV of the amplifier V converts the output signal V1 of the internal amplifier IVV of the amplifier V to digitized ones Sample values on a data line V2 between the control device µCV of the amplifier V and the analog-to-digital converter ADCV of the amplifier V. The control device µCV of the amplifier V and preferably stores these sample values in a memory MEMV of the amplifier V; via a memory data bus MEMDBV between the control device µCV of the amplifier V and the memory MEMV of the amplifier V. The control device µC of the deployable quantum computer QC can then access the data in the memory MEMV of the amplifier V via the control data bus SDB, the data interface VIF of the amplifier V, the internal control data bus SDBV of the amplifier V and the control device µCV of the amplifier V and further process it.

Figure 14Figure 14 shows an example of a garment with a deployable quantum computer system QUSYS. For rework, the document presented here refers to the document as an example WO 2020 239 172 A1 , which reveals a method for CMOS integration.

The document presented here proposes incorporating one or more quantum computers QC1, QC2 and a central control unit ZSE into the material of a garment KLST. The quantum computer system QUSYS preferably corresponds to the quantum computer system QUSYS 4 , 10 or 11 or similar. The item of clothing can also be a wristwatch or the like.

Figure 15

15 shows an example of a satellite or spacecraft as an example of a vehicle with a deployable quantum computer system QUSYS. The document presented here proposes integrating one or more quantum computers QC1, QC2 and a central control unit ZSE into the satellite or spacecraft. The quantum computer system QUSYS preferably corresponds to the quantum computer system QUSYS 4 , 10 or 11 or similar.

Figure 16

16 shows an example of a smartphone with a deployable QUSYS quantum computer system. The document presented here proposes integrating one or more quantum computers QC1, QC2 and a central control unit ZSE into the smartphone. For rework, the document presented here refers to the document as an example WO 2020 239 172 A1 , which reveals a method for CMOS integration. The quantum computer system QUSYS preferably corresponds to the quantum computer system QUSYS 4 , 10 or 11 or similar.

glossary

vehicle

A vehicle in the sense of the document presented here can also be a motor vehicle, a two-wheeler, a tricycle or a truck, a commercial vehicle, a robot, a transport vehicle, a drone, a robot drone, a missile, a floating body, a submersible body , a ship, a submarine, a sea mine, a landmine, a rocket, a projectile, a satellite, a space station, a trailer, a barge, a container, in particular a sea container and/or smartphone and/or a garment and/or a piece of jewelry and/or a wearable quantum computer system and/or a mobile quantum computer system and/or vehicle and/or robot and/or aircraft and/or a cruise missile and/or underwater vehicle and/or surface floating body and/or underwater floating body and/or or a mobile medical device and/or a deployable weapon system and/or warhead and/or surface or underwater vehicle and/or projectile and/or other mobile device and/or mobile device and/or the like. If the document presented here describes a specific vehicle, the description also includes and claims all other vehicles described above, as long as this makes sense in the relevant context. In particular, all applications to weapons and weapon systems and mobile medical devices, which can typically be relocated at least temporarily, are also included. In the sense of the document presented here, this document interprets the term vehicle very broadly as a “transportable device”, which may, in particular, temporarily have a vehicle has its own propulsion and/or means of transport on water and/or land and/or in the air and/or in space.

horizontal

The adjective “horizontal” is used in this disclosure as part of the name of the device parts and the associated sizes unless expressly stated otherwise. This happens because the quantum bits are numbered consecutively. This allows the columns (vertical) and rows (horizontal) to be better distinguished within two-dimensional quantum bit arrangements. A “horizontal line” is therefore a line within such a two- or one-dimensional arrangement that runs along a line. The assigned current is then referred to, for example, in an analogous manner as “horizontal line current” to give an example of naming a quantity.

Isotopically pure

A material is isotopically pure within the meaning of this disclosure if the concentration of isotopes other than the base isotopes that dominate the material is so low that the technical purpose is combined to an extent sufficient for the production and sale of products with an economically sufficient level Production yield is achieved. This means that interference caused by such isotopic impurities does not interfere with the functionality of the quantum bits, or at most only does so to a sufficiently small extent. In relation to diamond, this means that the diamond preferably consists essentially of ¹² C isotopes as base isotopes that have no magnetic moment.

Vicinity

For example, when this disclosure refers to a “device that is located near the plumb point (LOTP) or at the plumb point (LOTP) for generating a circularly polarized microwave field,” the term proximity is to be understood in this way that this device exerts or can exert an intended effect with its polarized microwave field or otherwise on the quantum dot (NV) located on the plumb line (LOT), which in turn is intended to be so in connection with the disclosure presented here It should be understood that the intended effect allows a procedural step to be carried out in the functional steps for the intended use of a device proposed here.

NP completeness

In computer science, a problem is called NP-complete (complete for the class of problems that can be solved nondeterministically in polynomial time) if it is one of the most difficult problems in the NP class, i.e. it is both in NP and NP-hard is. In colloquial terms, this means that it probably cannot be solved efficiently.

Formally, NP-completeness is only defined for decision problems (possible solutions only “yes” or “no”), while other types of problems are referred to as NP-equivalence (e.g. search problems or optimization problems). In colloquial language, however, this distinction is often not made, so that one generally speaks of “NP-complete problems”, regardless of whether a decision problem is present or not. This is possible because different problem types can be converted into one another (reducible to one another).

• • in der Komplexitätsklasse NP liegt: Ein deterministisch arbeitender Rechner benötigt nur polynomiell viel Zeit, um zu entscheiden, ob eine vorgeschlagene Lösung eines zugehörigen Suchproblems tatsächlich eine Lösung ist, und
• • zu den NP-schweren Problemen gehört: Alle anderen Probleme, deren Lösungen deterministisch in polynomieller Zeit überprüft werden können, können auf das Problem derart zurückgeführt werden, dass diese Rückführung auf einem deterministischen Rechner höchstens polynomielle Zeit in Anspruch nimmt. Man spricht von einer Polynomialzeitreduktion.

A decision problem is NP-complete if it

• • is in the complexity class NP: A deterministic computer only needs a polynomial amount of time to decide whether a proposed solution to an associated search problem is actually a solution, and
• • belongs to the NP-hard problems: All other problems whose solutions can be checked deterministically in polynomial time can be reduced to the problem in such a way that this reduction takes at most polynomial time on a deterministic computer. This is called a polynomial time reduction.

NP-complete problems probably cannot be solved efficiently because solving them on real computers takes a long time. In practice, this does not have a negative effect in every case, that is, for many NP-complete problems there are solution methods that can be used to solve them in an acceptable time for the sizes that occur in practice.

• • Für kein NP-vollständiges Problem konnte bisher nachgewiesen werden, dass es in polynomieller Zeit lösbar wäre.
• • Falls nur ein einziges dieser Probleme in polynomieller Zeit lösbar wäre, dann wäre jedes Problem in NP in polynomieller Zeit lösbar, was große Bedeutung für die Praxis haben könnte (jedoch nicht notwendigerweise haben muss).

Many important problems that arise in practice are NP-complete, which makes NP-completeness a central concept in computer science. This importance is further reinforced by the so-called P-NP problem:

• • No NP-complete problem has yet been shown to be solvable in polynomial time.
• • If only one of these problems were solvable in polynomial time, then every problem in NP would be solvable in polynomial time, which could (but does not necessarily have) great practical importance.

Since Cook's introduction of NP-completeness, completeness has been expanded into a general concept for arbitrary complexity classes.

Quantum computer program and quantum operation and quantum op-code

In the sense of the document presented here, a quantum computer program is a program that includes at least one quantum operation and is executed by a control device µC of a deployable quantum computer QC. One or more binary data in the memory NVN, RAM of the control device μC of the deployable quantum computer QC preferably encode such a quantum operation. For example, it can be a predetermined data word. A quantum operation in the sense of the document presented here manipulates at least the quantum state of at least one quantum dot of the quantum dots NV1, NV2, NV3 of the deployable quantum computer QC and/or manipulates at least the quantum state of at least one core quantum dot of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ of the deployable quantum computer QC. The technical teaching of the document presented here also refers to the data word that symbolizes such a quantum operation as a quantum op code. A quantum computer program therefore includes at least one quantum op-code. The quantum op code can also include multiple data words.

Pure substrate

A pure substrate within the meaning of this disclosure exists when the concentration of atoms other than the base atoms that dominate the material of the substrate is so low that the technical purpose is sufficient for the production and sale of products an economically sufficient production yield is achieved. This means that disruptions caused by such atomic impurities do not disrupt the functionality of the quantum bits, or at most only do so to a sufficiently small extent. In relation to diamond, this means that the diamond preferably consists essentially of carbon atoms and contains no or only an insignificant number of foreign atoms. The substrate preferably contains no ferromagnetic impurities such as Fe and/or Ni, as their magnetic fields can interact with the spin of the quantum dot (NV).

insignificant phase rotation

An insignificant phase rotation of the state vector of a quantum dot for the purposes of this disclosure is a phase rotation that can be considered insignificant or correctable for operation and functionality. As a first approximation, it can therefore be assumed to be slightly zero.

vertical

The adjective "vertical" is used in this disclosure as part of the name of the device parts and the associated dimensions unless expressly stated otherwise. This happens because the quantum bits are numbered consecutively. This allows the columns (vertical) and rows (horizontal) to be better distinguished within two-dimensional quantum bit arrangements. A “vertical line” is therefore a line within such a two- or one-dimensional arrangement that is routed along a column. The assigned current is then referred to, for example, in an analogous manner as “vertical line current” to give an example of naming a quantity.

Reference symbol list

ADCV

Amplifier V analog-to-digital converter;

AS

Shielding;

BENG

first energy reserve;

BENG2

second energy reserve;

BNV

rotating magnetic field;

BSC

back contact;

BTR

Energy reserve of the vehicle (submarine, motor vehicle, etc.);

CBA

control unit A;

CBB

control unit B;

CECEQUREG

nuclear-electron-nuclear-electron quantum register;

CEQUREG1

first nuclear-electron quantum register;

CEQUREG2

second core-electron quantum register;

CI1

first nuclear quantum dot. Preferably, the exemplary first core quantum dot CI1 is an isotope with a nuclear magnetic moment in the substrate D, wherein the substrate D in the region of the core quantum dot CI1 preferably comprises essentially or even more preferably absolutely no isotopes with a nuclear magnetic moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 .;

CI11

first core quantum point CI1 ₁ of the first quantum ALU QUALU1. The exemplary first core quantum dot CI1 ₁ of the first quantum ALU QUALU1 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI1 ₁ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The first core quantum point CI1 ₁ of the first quantum ALU QUALU1 is in the 3 not shown for clarity. The reader should assume that in the 3 the first core quantum point CI1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum point NV1 as in the 2 the first core quantum dot CI1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CI12

second core quantum point CI1 ₂ of the first quantum ALU QUALU1. The exemplary second core quantum dot CI1 ₂ of the first quantum ALU QUALU1 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI1 ₂ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The second core quantum point CI1 ₂ of the first quantum ALU QUALU1 is in the 3 not shown for clarity. The reader should assume that in the 3 the second core quantum point CI1 ₂ of the first quantum ALU QUALU1 is coupled to the first quantum point NV1 as in the 2 the second core quantum dot CI1 ₂ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CI13

third core quantum dot CI1 ₃ of the first quantum ALU QUALU1 Preferably, the exemplary third core quantum dot CI1 ₃ of the first quantum ALU QUALU1 is an isotope with a magnetic nuclear moment in the substrate D, the substrate D in the area of the core quantum dot CI1 ₃ preferably substantially or still more preferably comprises absolutely no isotopes with a nuclear magnetic moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The third core quantum point CI1 ₃ of the first quantum ALU QUALU1 is in the 3 not shown for clarity. The reader should assume that in the 3 the third core quantum point CI1 ₃ of the first quantum ALU QUALU1 is coupled to the first quantum point NV1 as in the 2 the third core quantum dot CI1 ₃ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CI2

second core quantum dot. Preferably, the exemplary second core quantum dot CI2 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the region of the core quantum dot CI2 preferably comprises essentially or even more preferably absolutely no isotopes with a magnetic nuclear moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 .;

CI21

first core quantum point CI2 ₁ of the second quantum ALU QUALU2. Preferably, the exemplary first core quantum dot CI2 ₁ of the second quantum ALU QUALU2 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI2 ₁ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The first core quantum point CI2 ₁ of the second quantum ALU QUALU2 is in the 3 not shown for clarity. The reader should assume that in the 3 the first core quantum point CI2 ₁ of the second quantum ALU QUALU2 is coupled to the second quantum point NV2 as in the 2 the first core quantum dot CI2 ₁ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2;

CI22

second core quantum point CI2 ₂ of the second quantum ALU QUALU2. The exemplary second core quantum dot CI2 ₂ of the second quantum ALU QUALU2 is preferably an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI2 ₂ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The second core quantum point CI2 ₂ of the second quantum ALU QUALU2 is in the 3 not shown for clarity. The reader should assume that in the 3 the second core quantum point CI2 ₂ of the second quantum ALU QUALU2 is coupled to the second quantum point NV2 as in the 2 the second core quantum dot CI2 ₂ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2;

CI23

third core quantum point CI2 ₃ of the second quantum ALU QUALU2. Preferably, the exemplary first core quantum dot CI2 ₃ of the second quantum ALU QUALU2 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI2 ₃ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The third core quantum point CI2 ₃ of the second quantum ALU QUALU2 is in the 3 not shown for clarity. The reader should assume that in the 3 the third core quantum point CI2 ₃ of the second quantum ALU QUALU2 is coupled to the second quantum point NV2 as in the 2 the third core quantum dot CI2 ₃ of the second quantum ALU QUALU2 is coupled to the second quantum dot NV2;

CI3

third core quantum dot. Preferably, the exemplary third core quantum dot CI3 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the region of the core quantum dot CI3 preferably comprises essentially or even more preferably absolutely no isotopes with a magnetic nuclear moment. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 ;

CI31

first core quantum point CI3 ₁ of the third quantum ALU QUALU3. Preferably, the exemplary first core quantum dot CI3 ₁ of the third quantum ALU QUALU3 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI3 ₁ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The first core quantum point CI3 ₁ of the third quantum ALU QUALU3 is in the 3 and in the 2 not shown for clarity. The reader should assume that in the 3 the first core quantum point CI3 ₁ of the third quantum ALU QUALU3 is coupled to the third quantum point NV3 as in the 2 the first core quantum dot CI1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CI32

second core quantum point CI3 ₂ of the third quantum ALU QUALU3. Preferably, the exemplary second core quantum dot CI3 ₂ of the third quantum ALU QUALU3 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI3 ₂ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The second core quantum point CI3 ₂ of the third quantum ALU QUALU3 is in the 3 and in the 2 not shown for clarity. The reader should assume that in the 3 the second core quantum point CI3 ₂ of the third quantum ALU QUALU3 is coupled to the third quantum point NV3 as in the 2 the second core quantum dot CI1 ₂ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CI33

third core quantum point CI3 ₃ of the third quantum ALU QUALU3. Preferably, the exemplary first core quantum dot CI3 ₃ of the third quantum ALU QUALU3 is an isotope with a magnetic nuclear moment in the substrate D, wherein the substrate D in the area of the core quantum dot CI3 ₃ preferably contains essentially or even more preferably absolutely no isotopes with a magnetic Core moment includes. In this context, the document presented here refers to the technical teachings already cited DE 10 2020 007 977 B4 . The third core quantum point CI3 ₃ of the third quantum ALU QUALU3 is in the 3 and in the 2 not shown for clarity. The reader should assume that in the 3 the third core quantum point CI3 ₃ of the third quantum ALU QUALU3 is coupled to the third quantum point NV3 as in the 2 the first core quantum dot CI1 ₁ of the first quantum ALU QUALU1 is coupled to the first quantum dot NV1;

CIF

first camera interface;

CIF2

second camera interface;

CM1

first camera;

CM2

second camera;

CPU

computer core;

D

substrate;

d1

first distance at which the first quantum dot NV1 is located below the surface OF of the substrate D;

d2

second distance at which the second quantum dot NV2 is located below the surface OF of the substrate D;

DBIF

data interface;

DBIFa

Data interface A;

DBIFb

data interface B;

DBS

dichroic mirror;

DEV

Energy supply of other device parts of the quantum computer QC, which typically also concerns device parts with other reference numbers. For a better overview, the power supply lines of the remaining device parts of the quantum computer QC are shown in the 1 not shown;

CLOSELY

propulsion of the vehicle;

ERS

energy system;

EXDB

external data bus;

EV

Power supply;

λfl

fluorescent radiation wavelength;

λpmp.

pump radiation wavelength;

FHB

factory hall or stationary device;

fHR

microwave and/or radio wave frequency;

FL

fluorescent radiation;

FLC

Fire control station. The fire control center can be a central control unit ZSE.

FLR

attitude control system;

FZ

Airplane;

FZT

aircraft carriers;

GDX

X control device for the translational positioning device in the X direction XT;

GDY

Y control device for the translational positioning device in the Y direction YT;

GH

Housing;

GPS

Navigation system or device for determining the position and/or orientation of the quantum computer QC. If necessary, the navigation system can also determine translational speeds and/or rotational speeds of the quantum computer QC and report them to the computer core CPU of the control device µC of the quantum computer QC via the internal data bus INTDB. If necessary, the navigation system can also determine translational accelerations and/or rotational accelerations of the quantum computer QC and report them to the computer core CPU of the control device µC of the quantum computer QC via the internal data bus INTDB;

HD1

first horizontal driver stage for controlling the first quantum dot NV1 to be controlled;

HD2

second horizontal driver stage for controlling the second quantum dot NV2 to be controlled;

HD3

third horizontal driver stage for driving the third quantum dot NV3 to be controlled;

HeCLCS

Closed Loop Helium Gas Cooling System;

HS1

first horizontal receiver stage HS1, which can form a unit with the first horizontal driver stage HD1, for controlling the first quantum dot NV1 to be controlled;

HS2

second horizontal receiver stage HS2, which can form a unit with the second horizontal driver stage HD2, for controlling the second quantum dot NV2 to be controlled;

HS3

third horizontal receiver stage HS3, which can form a unit with the third horizontal driver stage HD3, for controlling the third quantum dot NV3 to be controlled;

IH1

first horizontal stream. The first horizontal current is the electrical current that flows through the first horizontal line LH1.

IH2

second horizontal stream. The second horizontal current is the electrical current that flows through the second horizontal line LH2.

IH3

third horizontal stream. The third horizontal current is the electrical current that flows through the third horizontal line LH3.

Ip

Intensity of the pulses of the pulsed pump radiation LB from the light source LD;

IpHF

Amplitude I _pHF of a pulse of the temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ;

IS

Isolation;

ISH1

first horizontal shield current flowing through the first horizontal shield line SH1;

ISH2

second horizontal shield current current flowing through the second horizontal shield line SH2;

ISH3

third horizontal shield current current flowing through the third horizontal shield line SH3;

ISH4

fourth horizontal shield current current flowing through the fourth horizontal shield line SH4;

ISV1

first vertical shield current flowing through the first vertical shield line SV1;

ISV2

second vertical shield current flowing through the second vertical shield line SV2;

IV1

first vertical stream. The first vertical current is the electric current flowing through the first vertical line LV1;

IVV

internal amplifier within amplifier V;

automobile

Car as an example of a vehicle;

KH1

first horizontal contact of the first quantum bit QUB1 with the first quantum dot NV1. The first horizontal contact of the first quantum bit QUB1, for example, electrically connects the first horizontal shielding line SH1 in the first quantum bit QUB1 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KH2

second horizontal contact of the first quantum bit QUB1 with the first quantum dot NV1 and first horizontal contact of the second quantum bit QUB2 with the second quantum dot NV2. The first quantum bit QUB1 and the second quantum bit QUB2 use the in the example 3 this contact together. The contact, for example, electrically connects the second horizontal shielding line SH2 in the first quantum bit QUB1 and in the second quantum bit QUB2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KH3

second horizontal contact of the second quantum bit QUB2 with the second quantum dot NV2 and first horizontal contact of the third quantum bit QUB3 with the third quantum dot NV3. The second quantum bit QUB2 and the third quantum bit QUB3 use the in the example 3 this contact together. The contact, for example, electrically connects the third horizontal shielding line SH3 in the second quantum bit QUB2 and in the third quantum bit QUB3 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KH4

second horizontal contact of the third quantum bit QUB3 with the third quantum dot NV3. The contact, for example, electrically connects the fourth horizontal shielding line SH3 in the third quantum bit QUB3 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV11

first vertical contact of the first quantum bit QUB1 with the first quantum dot NV1. The first vertical contact of the first quantum bit QUB1 electrically connects the first vertical shielding line SV1 in the first quantum bit QUB1 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV12

second vertical contact of the first quantum bit QUB1 with the first quantum dot NV1. The second vertical contact of the first quantum bit QUB1 preferably electrically connects the second vertical shielding line SH2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV21

first vertical contact of the second quantum bit QUB2 with the second quantum dot NV2. The first vertical contact of the second quantum bit QUB2 electrically connects the first vertical shielding line SV1 in the second quantum bit QUB2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV22

second vertical contact of the second quantum bit QUB2 with the second quantum dot NV2. The second vertical contact of the second quantum bit QUB2 preferably electrically connects the second vertical shielding line SH2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV31

first vertical contact of the third quantum bit QUB3 with the third quantum dot NV3. The first vertical contact of the third quantum bit QUB3 electrically connects the first vertical shielding line SV1 in the third quantum bit QUB3 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV32

second vertical contact of the third quantum bit QUB3 with the third quantum dot NV3. The second vertical contact of the third quantum bit QUB3 preferably electrically connects the second vertical shielding line SH2 to the substrate D or the epitaxial layer DEPI. In the case of diamond, the substrate material is preferably a contact that comprises titanium or is made of titanium;

KV

relocatable cooler;

L.B

pump radiation;

LD

light source;

LDRV

light source driver;

LDV

loading device;

LH1

first horizontal line;

LH2

second horizontal line;

LH3

third horizontal line;

LM

Lamp with a light source;

LV1

first vertical line;

µC

control device;

µC1

first control device of the first quantum computer QC1;

µC1a

first control device A of the first quantum computer QC1;

pC1b

first control device B of the first quantum computer QC1;

pC2

second control device of the second quantum computer QC2;

pC3

third control device of the third quantum computer QC3;

µC4

fourth control device of the fourth quantum computer QC4;

µC5

fifth control device of the fifth quantum computer QC5;

µC6

sixth control device of the sixth quantum computer QC6;

µC7

seventh control device of the seventh quantum computer QC7;

µC8

eighth control device of the eighth quantum computer QC8;

µC9

ninth control device of the ninth quantum computer QC9;

µC10

tenth control device of the tenth quantum computer QC10;

µC11

eleventh control device of the eleventh quantum computer QC11;

µC12

twelfth control device of the twelfth quantum computer QC12;

µC13

thirteenth control device of the thirteenth quantum computer QC13;

µC14

fourteenth control device of the fourteenth quantum computer QC14;

µC15

fifteenth control device of the fifteenth quantum computer QC15;

µC16

sixteenth control device of the sixteenth quantum computer QC16;

µCV

Amplifier V control device;

MDBIF

internal data interface MDBIF;

MEMDBV

Memory data bus between control device µCV of amplifier V and memory MEMV of amplifier V;

MEMV

Amplifier V memory;

MFSx

first magnetic field control;

MFSy

second magnetic field control;

MFSz

third magnetic field control;

MGx

first magnetic field generating means, which preferably generates a magnetic flux density B _x , which preferably essentially has a direction which preferably corresponds to the first direction, for example the direction of the X axis;

MGy

second magnetic field generating means, which preferably generates a magnetic flux density B _y , which preferably essentially has a direction which preferably corresponds to the second direction, for example the direction of the Y axis;

MGz

third magnetic field generating means, which preferably generates a magnetic flux density B _z , which preferably essentially has a direction which preferably corresponds to the third direction, for example the direction of the Y axis;

MSx

Magnetic field sensor for the magnetic flux density B _x in the direction of the X axis;

MSy

Magnetic field sensor for the magnetic flux density B _y in the direction of the Y axis;

MSz

Magnetic field sensor for the magnetic flux density B _z in the direction of the Z axis;

mWA

microwave and/or radio wave antenna;

MW/RF AWFG

Microwave and/or radio wave frequency generator for generating largely freely definable waveforms (English: arbitrary wave form generator);

NAV

navigation system and/or autopilot;

NV1

first quantum dot. Preferably, the exemplary first quantum dot NV1 is a paramagnetic center in the substrate D. Preferably, the exemplary first quantum dot NV1 is an NV center or a SiV center or an ST1 center in the substrate D;

NV2

second quantum dot. Preferably, the exemplary second quantum dot NV2 is a paramagnetic center in the substrate D. Preferably, the exemplary second quantum dot NV2 is an NV center or a SiV center or an ST1 center in the substrate D;

NV3

third quantum dot. Preferably, the exemplary third quantum dot NV3 is a paramagnetic center in the substrate D. Preferably, the exemplary third quantum dot NV3 is an NV center or a SiV center or an ST1 center in the substrate D;

NVM

non-volatile memory;

OF

Surface;

O.S

optical system;

OSZ

Clock of the computer core CPU of the control device µC of the quantum computer QC;

P.D

photodetector;

PM

permanent magnet;

PV

Positioning device for the permanent magnet PM;

PVC

Control device for the positioning device PV for the permanent magnet PM;

PWR

Energy supply to the charging device LDV;

QC

quantum computers;

QC1

first quantum computer;

QC2

second quantum computer;

QC3

third quantum computer;

QC4

fourth quantum computer;

QC5

fifth quantum computer;

QC6

sixth quantum computer;

QC7

seventh quantum computer;

QC8

eighth quantum computer;

QC9

ninth quantum computer;

QC10

tenth quantum computer;

QC11

eleventh quantum computer;

QC12

twelfth quantum computer;

QC13

thirteenth quantum computer;

QC14

fourteenth quantum computer;

QC15

fifteenth quantum computer;

QC16

sixteenth quantum computer;

QCTV

Quantum computer system separation device. The quantum computer system separation device preferably separates an external data bus EXTDB, which, for example, connects a first quantum computer system QUSYS with a second quantum computer system QUSYS, if necessary, so that the quantum computer system QUSYS, which previously included the first and the second quantum computer system QUSYS, breaks down into two separate quantum computer systems QUSYS due to the separation. However, the quantum computer system separation device can also connect a previously separate first quantum computer system QUSYS with a previously separate second quantum computer system QUSYS and, if necessary, couple them, so that the quantum computer system QUSYS is created, which then comprises the first and second quantum computer systems QUSYS by connecting these two quantum computer systems via quantum computer system separation device into one Quantum computer system QUSYS merges;

QUALU1

first quantum ALU. The exemplary first quantum ALU consists of a first quantum point NV1 and a first core quantum point CI1 ₁ of the first quantum ALU and a second core quantum point CI1 ₂ of the first quantum ALU and a third core quantum point CI1 ₃ of the first quantum ALU ( 2 );

QUALU2

second quantum ALU. The exemplary second quantum ALU consists of a second quantum point NV2 and a first core quantum point CI2 ₁ of the second quantum ALU and a second core quantum point CI2 _z of the second quantum ALU and a third core quantum point CI2 ₃ of the second quantum ALU ( 2 );

QUSYS

deployable quantum computing system;

R.A.M.

volatile memory;

RKT

Rocket. The rocket is just an example of a possible payload. The payload itself can include one or more QUSYS quantum computer systems. Preferably, the quantum computer system QUSYS of the payload is connected to the quantum computer system QUSYS of the vehicle FZ, or the object in which the payload is set up or stored, for example via an external data bus EXTDB during the time of the payload;

RKTC

missile launch control;

50

receiver output signal;

S1

reception signal;

S4

measured value signal;

S5

broadcast signal;

SC

Sea containers. The sea container is just one example of a transportable container in which one or more QUSYS quantum computer systems or one or more QC quantum computers can be operated;

SCHR

ship propeller;

SDB

control data bus;

SDBV

internal control data bus within the amplifier V;

SENS

one or more sensors;

SH1

first horizontal shield line;

SH2

second horizontal shield line;

SH3

third horizontal shield line;

SH4

fourth horizontal shield line;

SRG

first energy processing device, in particular a voltage converter or a voltage regulator or a current regulator;

SRG2

second energy processing device, in particular a voltage converter or a voltage regulator or a current regulator;

ST

temperature sensor;

STM

semi-transparent mirror;

SUB

submarine;

SV1

first horizontal shield line;

SV2

second vertical shield line;

TL

Low loader. The low loader is an example of a vehicle without its own propulsion.

TRP

torpedoes;

TRPC

torpedo launch control;

T.S

separator;

T0HF

Reference time of a pulse of the pulsed electromagnetic field with microwave and/or radio wave frequency f _HF . Preferably, the reference time t _0HF is equal to the reference time t _0P for a pulse sequence or at a fixed time interval from the reference time for a pulse sequence t _0p ;

t0p

Reference time for a pulse sequence. Preferably, the reference time t _0p for a pulse sequence is equal to the reference time t _OHF or at a fixed time interval from the reference time t _0HF ;

tdp

the time duration t _dp of the pulses of the pulsed pump radiation LB of the light source LD;

tdHF

temporal pulse duration of the pulse of the pulsed electromagnetic field with microwave and/or radio wave frequency f _HF . It is the temporal pulse duration of the temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , C13 ₃ in pulse form;

tsp

Temporal position of the pulses of the pulsed pump radiation LB of the light source LD relative to a reference time t ₀ As a rule, the temporal position t _sp of a pulse denotes the starting time of the relevant pulse;

tspHF

Pulse start time t _spHF relative to the reference time t _0HF of a pulse of the temporal envelope curve of the radiation of an electromagnetic field by the one or more devices MW/RF-AWFG for generating an electromagnetic wave field at the respective location of the quantum dots NV1, NV2, NV3 and at the respective location of the core quantum dots CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ;

UDB1

first sub-data bus;

UDB2

second sub-data bus;

UDB3

third sub-data bus;

UDB4

fourth sub-data bus;

ÜOSZ

Monitoring clock generation of the quantum computer monitoring device QUV of the quantum computer QC;

US

bottom of substrate D;

v

Amplifier;

V1

Output signal of the internal amplifier IVV of the amplifier V and input signal of the analog-to-digital converter ADCV of the amplifier V;

V2

Data line between the control device µCV of the amplifier V and the analog-to-digital converter ADCV of the amplifier V;

Vbatext

electrical energy from an external power supply, for example an external power supply;

VD1

first vertical driver stage for controlling the quantum dots NV1, NV2, NV3 to be controlled;

VIF

Data interface of the amplifier V to the control data bus SDB;

VS1

first vertical receiver stage, which can form a unit with the first vertical driver stage VD1, for controlling the first quantum dots NV1, NV2, NV3 to be controlled;

WFG

waveform generator;

XT

translational positioning device in the X direction;

YT

translational positioning device in Y direction;

ZM

Tractor. The tractor is an example of a drive for a container with one or more quantum computers QC and/or one or more quantum computer systems QUSYS, which can be separated from the container or added to the container. In the example of the 6b the container is an exemplary low-loader TL with a sea container SC;

ZSE

central control unit;

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Claims (11)

Deployable quantum computer (QC) in a mobile device, in particular for use in a smartphone or a portable quantum computer system (QUSYS) or in a vehicle or in a deployable weapon system, - with a substrate (D) and - with one or more quantum dots (NV1, NV2, NV3) and - with a light source (LD) and - with a light source driver (LDRV) and - with one or more devices (mWA, MW/RF-AWFG) for generating an electromagnetic wave field at the respective location of the quantum dots (NV1, NV2 , NV3) and - with a control device (µC) and - with one or more memories (RAM, NVM) of the control device (µC) and - with a waveform generator (WFG) and - with an optical system (OS) and - with a quantum state readout device , - wherein the quantum state readout device - can comprise a device for optically reading out the quantum states, in particular a photodetector (PD) and an amplifier (V), and / or - a device for electronically reading out the states of the quantum dots (NV1, NV2, NV3). can, and - where the quantum dots (NV1, NV2, NV3) are located in the substrate (D) and - where the substrate (D) is doped so that the Fermi level in the area of the quantum dots (NV1, NV2, NV3) is like this is shifted so that the quantum dots (NV1, NV2, NV3) are electrically charged, and - the waveform generator (WFG) generates the light source control signal (S5) and - the light source driver (LDRV) controls the light source (LD) depending on a light source control signal ( S5) is supplied with electrical energy and - the control device (µC) controls the waveform generator (WFG) and - the light source (LD) supplies the quantum dot or the multiple quantum dots (NV1, NV2, NV3) with pump radiation by means of the optical system (OS). (LB) of a pump radiation wavelength (λ _pmp ) and - wherein the one or more quantum dots (NV1, NV2, NV3) emit fluorescent radiation (FL) with a fluorescent radiation wavelength (λ _fl ) upon irradiation with electromagnetic radiation of the pump radiation wavelength (λ _pmp ). and - wherein the photodetector (PD) detects at least part of the fluorescence radiation (FL) by means of the optical system (OS) and converts a receiver output signal (S0) and - wherein the amplifier (V) converts the receiver output signal (S0) into a received signal (S1) amplifies and filters and/or wherein the device for electronically reading out the states of the quantum dots (NV1, NV2, NV3) generates a received signal (S1) and - in particular the received signal (S1) can be present in the form of digital sample values within the amplifier (V). and - wherein the control device (µC) controls one or more devices (mWA, MW/RF-AWFG) for generating an electromagnetic wave field at the respective location of the quantum dots (NV1, NV2, NV3) and - wherein the control device (µC) by control one or more devices (mWA, MW/RF-AWFG) for generating an electromagnetic wave field at the respective location of the quantum dots (NV1, NV2, NV3) and/or by controlling the emission of the light source (LD) states of the quantum dots (NV1, NV2 , NV3) can change and/or couple with each other and - wherein the control device (µC) has means to generate or calculate a measured value signal (S4) with one or more measured values from one or more received signals (S1), the measured value signal (S4) can also be just a measured value, and - where the measured value signal (S4) depends on states of quantum dots (NV1, NV2, NV3), characterized in that - the deployable quantum computer (QC) and / or the mobile device has a deployable energy supply (LDV, TS, BENG, SRG) for supplying at least some of the sub-devices of the quantum computer (QC) with energy and - wherein the relocatable energy supply (LDV, TS, BENG, SRG) is a mobile energy supply (LDV, TS, BENG) and an energy processing device (SRG), in particular a voltage converter or a voltage regulator or a current regulator. Deployable quantum computer (QC). Claim 1 - with one or more nuclear quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) and - wherein the one or more devices (mWA, MW/RF -AWFG) for generating an electromagnetic wave field at the respective location of the quantum dots (NV1, NV2, NV3) and at the same time one or more devices (mWA, MW/RF-AWFG) for generating an electromagnetic wave field at the respective location of the core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 _{3 , CI3 1 ,} CI3 ₂ , CI3 ₃ ) and - where the quantum dots (NV1, NV2, NV3) and the nuclear core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 3 , CI3 ₁ , CI3 ₂ , CI3 ₃ ) are located in _the common substrate (D) and - wherein the control device (µC) controls the one or more devices for generating an electromagnetic wave field and - wherein the control device (µC) by controlling the one or more devices for generating an electromagnetic wave field and / or by controlling the emission of the light source (LD) - states the quantum dots (NV1, NV2, NV3) and / or core quantum dots (CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3a) can change and/or - can couple quantum dots (NV1, NV2, NV3) with other quantum dots (NV1, NV2, NV3). and/or - quantum dots (NV1, NV2, NV3) can couple to core quantum dots (CI1 ₁ , C11 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) and/or - core quantum dots ( CI1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) with other core quantum dots (Cl1 ₁ , CI1 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , Cl3 ₃ ), - the measured value signal (S4) of states of quantum dots (NV1, NV2, NV3) and/or of states of core quantum dots (CI1 ₁ , C11 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) depends. Deployable quantum computer (QC). Claim 1 or 2 - wherein the mobile energy supply (LDV, TS, BENG) supplies the energy processing device (SRG) with energy and - wherein the energy processing device (SRG) supplies other device parts of the quantum computer (QC) with electrical energy. Deployable quantum computer (QC) according to one of the Claims 1 until 3 , wherein the mobile energy supply (LDV, TS, BENG) has a charging device (LDV) and a separation device (TS) and an energy reserve (BENG) and wherein the quantum computer (QC) has a first operating mode and a second operating mode and wherein in the first Operating mode - firstly, the separating device (TS) connects the charging device (LDV) with the energy reserve (BENG) and - secondly, the charging device (LDV) charges the energy reserve (BENG) with electrical energy from an external energy supply (V _batext ) and / or where in the first operating mode - firstly, the separating device (TS) connects the charging device (LDV) with the energy processing device (SRG) and - secondly, the charging device (LDV) supplies the energy processing device (SRG) with electrical energy from an external energy supply (V _batext ) and /or wherein in the second operating mode - firstly, the separating device (TS) separates the charging device (LDV) from the energy reserve (BENG) and - secondly, the separating device (TS) separates the charging device (LDV) from the energy processing device (SRG) and - Thirdly, the energy reserve (BENG) supplies the energy processing device (SRG) with electrical energy. Deployable quantum computer (QC) according to one of the Claims 1 until 4 - wherein the deployable quantum computer (QC) and all the necessary means for operating this deployable quantum computer (QC) are part of a mobile device and - wherein these means for operating the deployable quantum computer (QC) are also deployable and wherein these means are used to operate the deployable quantum computer (QC) are part of the quantum computer (QC) and - these means for operating the deployable quantum computer (QC) are also part of the mobile device and - it is irrelevant whether the operation of the deployable quantum computer (QC) despite the presence of all the resources for operating the deployable quantum computer (QC) as part of the deployable quantum computer (QC) is coupled to means and/or commands from outside the deployable quantum computer (QC). Deployable quantum computer (QC) according to one of the Claims 1 until 5 , - wherein the deployable quantum computer (QC) has one or more deployable cooling devices (KV), which can be deployed together with the deployable quantum computer (QC), and - wherein one or more of the deployable cooling devices (KV) are suitable and / or provided for this purpose , the spin temperature of quantum dots (NV1, NV2, NV3) and/or of core quantum dots (CI1 ₁ , C11 ₂ , CI1 ₃ , CI2 ₁ , CI2 ₂ , CI2 ₃ , CI3 ₁ , CI3 ₂ , CI3 ₃ ) and/or to lower the temperature of the substrate (D). Smartphone and/or a portable quantum computing system (QUSYS) and/or a mobile quantum computing system (QUSYS) and/or vehicle and/or robot and/or aircraft and/or missile and/or satellite and/or a rum missile and/or space station and/ or floating body and/or ship and/or underwater vehicle and/or surface floating body and/or underwater floating body and/or deployable weapon system and/or warhead and/or surface or underwater vehicle and/or Projectile and/or other mobile device and/or movable device, - wherein the claim presented here and the claims dependent on it all refer to these hereinafter as a vehicle and - wherein the vehicle is a deployable quantum computer (QC) according to one or more of the preceding Claims 1 until 6 comprises or - wherein the deployable quantum computer (QC) according to one or more of the preceding Claims 1 until 6 the vehicle includes. Vehicle after Claim 7 - wherein the vehicle transmits sensors and/or measuring devices, the measured values about the environment of the vehicle and/or states of the vehicle and/or states of the vehicle occupants or users of the vehicle and/or states of the vehicle's payload to the control device (µC) deliver, includes and/or - wherein the control device (µC) receives measured values about the environment of the vehicle via the data interface (DBIF) and/or - wherein the quantum computer (QC) makes a situation assessment for the overall condition of the vehicle depending on these measured values and/ or the surroundings of the vehicle and - whereby the overall condition of the vehicle can include the condition of the surroundings of the vehicle and / or the condition of the vehicle occupants and / or the condition of a payload of the vehicle. Vehicle after Claim 7 and/or 8 - wherein the quantum computer (QC) controls the vehicle and/or device parts of the vehicle as a function of these measured values and/or influences a control of the vehicle or a device part of the vehicle. Vehicle according to one or more of the preceding Claims 7 until 9 - the vehicle is a weapon system and/or - the vehicle comprises a weapon system that is coupled to the quantum computer (QC). Vehicle after Claim 10 - wherein the vehicle comprises a fire control system and - wherein the fire control system comprises the quantum computer (QC) or is coupled to the quantum computer (QC) and - wherein the control of the weapon system by the fire control system depends at least temporarily on the quantum computer (QC) or in cooperation with happens to the quantum computer (QC).

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