CN105301472A - Space single-particle turning rate measurement system - Google Patents

Space single-particle turning rate measurement system Download PDF

Info

Publication number
CN105301472A
CN105301472A CN201510741909.7A CN201510741909A CN105301472A CN 105301472 A CN105301472 A CN 105301472A CN 201510741909 A CN201510741909 A CN 201510741909A CN 105301472 A CN105301472 A CN 105301472A
Authority
CN
China
Prior art keywords
cpu
sram
flouride
radiation
under test
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201510741909.7A
Other languages
Chinese (zh)
Inventor
张楠
朱天成
李鑫
侯俊马
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Jinhang Computing Technology Research Institute
Original Assignee
Tianjin Jinhang Computing Technology Research Institute
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tianjin Jinhang Computing Technology Research Institute filed Critical Tianjin Jinhang Computing Technology Research Institute
Priority to CN201510741909.7A priority Critical patent/CN105301472A/en
Publication of CN105301472A publication Critical patent/CN105301472A/en
Pending legal-status Critical Current

Links

Landscapes

  • Measurement Of Radiation (AREA)

Abstract

The invention discloses a space single-particle turning rate measurement system. A member to be detected is connected to a CPU through a socket; a radiation resistance SRAM is connected to a CPU which is connected to a microcomputer; a radiation plate is positioned on sides of the member to be detected and the radiation resistance; before the radiation plate radiates, the CPU synchronically writes the same data into each byte of the radiation resistance SRAM and the member to be detected; in the radiation process of the radiation plate, the CPU circularly monitors the data stored in all units of the member to be detected, compares the data of the member to be detected with the data in the radiation resistance SRAM, performs statistics on the bits and the address of various bits and outputs the result obtained by the CPU to the microcomputer to display. The space single-particle turning rate measurement system can perform evaluation on the SEU reinforcement resistance technology in the practical environment, can perform monitoring verification on the SEU reinforcement resistance technology and can perform measurement on the single-particle turning rate of various members under various radiation environments.

Description

The measuring system of a kind of space single event upset rate
Technical field
The invention belongs to the fields of measurement of radioresistance technical merit, relate to the measuring system of a kind of space single event upset rate.
Background technology
There is a large amount of high energy particle in space radiation environment, can cause semiconductor devices generation single particle effect, has a strong impact on reliability and the life-span of product.When a high energy particle is injected in semiconductor, its can by with electronics and nuclear collision off-energy, ionize out a large amount of electron-hole pair simultaneously.If ionization occurs in the sensitizing range of circuit, as reverse biased pn junction, most of electron-hole pairs that its ionization produces by electric field separates, will be collected by drift, diffusion, funnelling or ion shunt effect.When the electric charge collected exceedes lowest charge (critical charge) needed for the change of circuit node logic state, single-particle inversion (SEU) will occur.
Primary particle inversion resistant reinforcing safeguards technique is the technology summation guaranteeing that element, module, subsystem or system normally can work under particular radiation environment, comprises technology, method for organizing, document management, process management etc.In a project, Radiation hardness assurance technology consider more late, so pinpoint the problems caused impact and cost also larger.To the checking of reinforcement measure in Radiation hardness assurance technology, judge whether radiation resisting capability of device satisfies the demands very important.The assessment to anti-single particle overturn reinforcement technique is carried out at present mainly through calculating single event upset rate.At present, at home and abroad association area does not measure the description of single event upset rate.
Summary of the invention
(1) goal of the invention
The object of the present invention is to provide a kind of system can measuring chip single event upset rate under particular space radiation environment, thus be that primary particle inversion resistant reinforcement technique proposes a kind of effective appraisal procedure.
(2) technical scheme
In order to solve the problems of the technologies described above, the invention provides the measuring system of a kind of space single event upset rate, it comprises: device under test, Flouride-resistani acid phesphatase SRAM, irradiation plate, CPU and microcomputer; Device under test connects CPU by socket, and Flouride-resistani acid phesphatase SRAM connects CPU, CPU connected with computer, and irradiation plate is arranged on device under test and Flouride-resistani acid phesphatase SRAM side; At irradiation plate predose, CPU is synchronized to Flouride-resistani acid phesphatase SRAM and each byte of device under test writes identical data; In irradiation plate irradiation process, the data stored in all unit of CPU circulatory monitoring device under test, and compared with data in Flouride-resistani acid phesphatase SRAM, add up figure place and the address of not coordination, the result obtained by CPU outputs in microcomputer and shows; If device under test is not identical with data in Flouride-resistani acid phesphatase SRAM, then there occurs single-particle inversion, record and add up upset number and address thereof, obtaining total upset number and the upset situation in a certain moment.
Wherein, connected between described CPU and microcomputer by serial ports, cable between the two meets the distance needs between irradiation space and microcomputer position.
Wherein, described irradiation plate radiation can comprise the various high energy particles of heavy ion, high energy proton, can separately or mixed radiation, and radiation parameter is adjustable as required.
Wherein, described device under test is semiconductor devices; Described Flouride-resistani acid phesphatase SRAM Flouride-resistani acid phesphatase upset rate is zero.
(3) beneficial effect
The measuring system of the space single event upset rate that technique scheme provides, can resist SEU reinforcement technique and assess in actual environment; SEU reinforcement technique can be resisted and carry out Real-Time Monitoring checking; The single event upset rate of multiple device under multiple radiation environment can be measured.
Accompanying drawing explanation
Fig. 1 is the theory diagram of the measuring system of embodiment of the present invention space single event upset rate.
Embodiment
For making object of the present invention, content and advantage clearly, below in conjunction with drawings and Examples, the specific embodiment of the present invention is described in further detail.
With reference to shown in Fig. 1, the measuring system of the present embodiment space single event upset rate is under irradiation plate radiation environment, measure the measuring system of device under test single event upset rate on socket, it comprises device under test, Flouride-resistani acid phesphatase SRAM (StaticRAM, static RAM), irradiation plate, CPU and microcomputer; Device under test connects CPU by socket, and Flouride-resistani acid phesphatase SRAM connects CPU, CPU connected with computer, and irradiation plate is arranged on device under test and Flouride-resistani acid phesphatase SRAM side; At irradiation plate predose, CPU is synchronized to Flouride-resistani acid phesphatase SRAM and each byte of device under test writes identical data, to write data be " AA " data, the binary data that namely " 0 " and " 1 " is spaced; In irradiation plate irradiation process, the data stored in all unit of CPU circulatory monitoring device under test, and compared with data in Flouride-resistani acid phesphatase SRAM, add up figure place and the address of not coordination, the result obtained by CPU outputs in microcomputer and shows.If device under test is identical with data in Flouride-resistani acid phesphatase SRAM, namely thinks and there occurs single-particle inversion, record and add up upset number and address thereof, total upset number can be obtained, the upset situation in a certain moment can be obtained again.
Connected by serial ports between CPU and microcomputer, usual connecting cable is set to tens meters long, to meet the long distance needs between irradiation space and microcomputer position.
The radiation-curable various high energy particles comprising heavy ion and high energy proton etc. of irradiation plate described in the present embodiment, can separately or mixed radiation, and the parameters such as radiation dose can be arranged as required.Before starting to measure Single Event Upset rate, the parameters such as the radiating particle of setting irradiation plate and radiation dose.
In the present embodiment, device under test is connected by socket, device under test is semiconductor devices, the semiconductor devices of this socket adaptive multiple encapsulation as much as possible, socket is that the test of semiconductor devices brings sizable facility, socket described in the present embodiment depends on the encapsulation of device under test, such as, chip to be measured is BGA484 encapsulation, and so in design, socket is just corresponding construction; Then CPU synchronously reads and writes and cycle detection this device, by the result of detection and the comparison of benchmark single event upset rate, thus obtain the single event upset rate of device under test under this kind of radiation environment, judge whether device primary particle inversion resistant irradiation technique used meets the requirements.
It is zero that Flouride-resistani acid phesphatase SRAM described in the present embodiment realizes Flouride-resistani acid phesphatase upset rate substantially.SRAM is the key components of space electronic system, and nearly all electronic system all uses SRAM memory as data storage carrier.But SRAM memory belongs to single particle effect Sensitive Apparatus, single-particle inversion can cause loss of data and instruction to make mistakes.Along with SRAM memory integrated level improves constantly, device feature size is more and more less, and critical charge is fewer and feweri, and single particle effect is further serious.
As can be seen from technique scheme, the present invention is by adopting irradiation plate irradiation Flouride-resistani acid phesphatase SRAM and device under test, and internal data both detecting by means of CPU also contrasts, to determine the single event upset rate of device under test, simple to operate, accuracy rate is high, applied widely.
The above is only the preferred embodiment of the present invention; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the technology of the present invention principle; can also make some improvement and distortion, these improve and distortion also should be considered as protection scope of the present invention.

Claims (4)

1. a measuring system for space single event upset rate, is characterized in that, comprising: device under test, Flouride-resistani acid phesphatase SRAM, irradiation plate, CPU and microcomputer; Device under test connects CPU by socket, and Flouride-resistani acid phesphatase SRAM connects CPU, CPU connected with computer, and irradiation plate is arranged on device under test and Flouride-resistani acid phesphatase SRAM side; At irradiation plate predose, CPU is synchronized to Flouride-resistani acid phesphatase SRAM and each byte of device under test writes identical data; In irradiation plate irradiation process, the data stored in all unit of CPU circulatory monitoring device under test, and compared with data in Flouride-resistani acid phesphatase SRAM, add up figure place and the address of not coordination, the result obtained by CPU outputs in microcomputer and shows; If device under test is not identical with data in Flouride-resistani acid phesphatase SRAM, then there occurs single-particle inversion, record and add up upset number and address thereof, obtaining total upset number and the upset situation in a certain moment.
2. the measuring system of space as claimed in claim 1 single event upset rate, it is characterized in that, connected between described CPU and microcomputer by serial ports, cable between the two meets the distance needs between irradiation space and microcomputer position.
3. the measuring system of space as claimed in claim 1 single event upset rate, is characterized in that, described irradiation plate radiation can comprise the various high energy particles of heavy ion, high energy proton, can separately or mixed radiation, and radiation parameter is adjustable as required.
4. the measuring system of the space single event upset rate according to any one of claim 1-3, is characterized in that, described device under test is semiconductor devices; Described Flouride-resistani acid phesphatase SRAM Flouride-resistani acid phesphatase upset rate is zero.
CN201510741909.7A 2015-11-04 2015-11-04 Space single-particle turning rate measurement system Pending CN105301472A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510741909.7A CN105301472A (en) 2015-11-04 2015-11-04 Space single-particle turning rate measurement system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510741909.7A CN105301472A (en) 2015-11-04 2015-11-04 Space single-particle turning rate measurement system

Publications (1)

Publication Number Publication Date
CN105301472A true CN105301472A (en) 2016-02-03

Family

ID=55198967

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510741909.7A Pending CN105301472A (en) 2015-11-04 2015-11-04 Space single-particle turning rate measurement system

Country Status (1)

Country Link
CN (1) CN105301472A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109991531A (en) * 2019-03-28 2019-07-09 西北核技术研究所 Atmospheric neutron single particle effect section gauge system and method under the conditions of low probability
CN112951314A (en) * 2021-02-01 2021-06-11 上海航天计算机技术研究所 Loadable general RAM self-testing method based on TSC695 processor
CN115356609A (en) * 2022-08-11 2022-11-18 中国科学院近代物理研究所 Method and system for improving single event upset resistance effect of active delay filter device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61262633A (en) * 1985-05-17 1986-11-20 Dan Kagaku:Kk Apparatus for measuring suspended fine particles
JP2008004597A (en) * 2006-06-20 2008-01-10 Canon Inc Charged particle beam drawing method, aligner, and process for fabricating device
CN101458299A (en) * 2008-12-31 2009-06-17 成都华微电子系统有限公司 On site programmable gate array single particle effect test method
CN103440185A (en) * 2013-07-22 2013-12-11 西安空间无线电技术研究所 Digital signal processing (DSP) device single particle turning effect testing method
CN104007382A (en) * 2013-02-20 2014-08-27 英特尔公司 High dose radiation detector

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61262633A (en) * 1985-05-17 1986-11-20 Dan Kagaku:Kk Apparatus for measuring suspended fine particles
JP2008004597A (en) * 2006-06-20 2008-01-10 Canon Inc Charged particle beam drawing method, aligner, and process for fabricating device
CN101458299A (en) * 2008-12-31 2009-06-17 成都华微电子系统有限公司 On site programmable gate array single particle effect test method
CN104007382A (en) * 2013-02-20 2014-08-27 英特尔公司 High dose radiation detector
CN103440185A (en) * 2013-07-22 2013-12-11 西安空间无线电技术研究所 Digital signal processing (DSP) device single particle turning effect testing method

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109991531A (en) * 2019-03-28 2019-07-09 西北核技术研究所 Atmospheric neutron single particle effect section gauge system and method under the conditions of low probability
CN109991531B (en) * 2019-03-28 2021-12-24 西北核技术研究所 Method for measuring atmospheric neutron single event effect cross section under low probability condition
CN112951314A (en) * 2021-02-01 2021-06-11 上海航天计算机技术研究所 Loadable general RAM self-testing method based on TSC695 processor
CN115356609A (en) * 2022-08-11 2022-11-18 中国科学院近代物理研究所 Method and system for improving single event upset resistance effect of active delay filter device
CN115356609B (en) * 2022-08-11 2023-05-26 中国科学院近代物理研究所 Method and system for improving single event upset resistance effect of active delay filter

Similar Documents

Publication Publication Date Title
CN102928773B (en) Method for testing proton/single event effect resisting capacity of device
CN102183779B (en) Multidirectional high energy particle detector
CN103605835B (en) Design evaluation method of spacecraft system-level anti-single particles
CN101458299A (en) On site programmable gate array single particle effect test method
CN105301472A (en) Space single-particle turning rate measurement system
CN102879730A (en) Single event upset characteristic testing method for partially triple modular redundancy reinforced SRAM (static random access memory) type FPGA (field programmable gate array)
CN104881519A (en) Single-event upset effect distinguishing method based on circuit simulation
Maillard et al. Single-event upsets characterization & evaluation of xilinx ultrascale™ soft error mitigation (sem ip) tool
Adcox et al. Construction and performance of the PHENIX pad chambers
Leite et al. Ionizing radiation effects on a COTS low-cost RISC microcontroller
CN108646284A (en) A kind of gamma spectrum combined detection system and gamma spectrum measurement method
Dandoy et al. Irradiation testing of ASICs for the HL-LHC ATLAS ITk Strip Detector
CN108287302A (en) The single particle effect detection circuit structure of space-oriented radiation environment
CN1760676B (en) Detector and method for detecting capability of microprocessor for anti event of single particle
CN111366968B (en) Heavy ion beam uniformity testing system and method
CN105866659B (en) A kind of more transient pulse distribution measurement methods of universal single-particle
Ytre-Hauge et al. Design and characterization of an SRAM-based neutron detector for particle therapy
Wu et al. MBU-Calc: A compact model for multi-bit upset (MBU) SER estimation
Sharma et al. Impact of gamma radiation on 8051 microcontroller performance
CN210427718U (en) Chip for quickly verifying combinational logic single event effect
US20220252743A1 (en) Nuclear reaction detection apparatus, method and program
Wall et al. Irradiation testing of ASICs for the ATLAS HL-LHC upgrade
Vasil’ev et al. Detector Part of the Station for the Research and Irradiation of Promising Products of Semiconductor Micro-and Nanoelectronics with High-Energy Ion Beams
CN112285758A (en) Nuclear radiation field probe, detector and detection system
CN109991531A (en) Atmospheric neutron single particle effect section gauge system and method under the conditions of low probability

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160203

WD01 Invention patent application deemed withdrawn after publication