CN118169763A - Unmanned plane-based geological exploration instrument, method and medium - Google Patents

Unmanned plane-based geological exploration instrument, method and medium Download PDF

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Publication number
CN118169763A
CN118169763A CN202410181798.8A CN202410181798A CN118169763A CN 118169763 A CN118169763 A CN 118169763A CN 202410181798 A CN202410181798 A CN 202410181798A CN 118169763 A CN118169763 A CN 118169763A
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CN
China
Prior art keywords
signal
coil
aerial vehicle
unmanned aerial
receiving
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CN202410181798.8A
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Chinese (zh)
Inventor
梁华睿
黄文轩
梁庆九
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Huarui Geosciences & Technology Co ltd Cug Wuhan
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Huarui Geosciences & Technology Co ltd Cug Wuhan
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Priority to CN202410181798.8A priority Critical patent/CN118169763A/en
Publication of CN118169763A publication Critical patent/CN118169763A/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01VGEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V3/00Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
    • G01V3/08Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation operating with magnetic or electric fields produced or modified by objects or geological structures or by detecting devices
    • G01V3/083Controlled source electromagnetic [CSEM] surveying
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01VGEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V3/00Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
    • G01V3/15Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation specially adapted for use during transport, e.g. by a person, vehicle or boat
    • G01V3/16Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation specially adapted for use during transport, e.g. by a person, vehicle or boat specially adapted for use from aircraft
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01VGEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V3/00Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
    • G01V3/38Processing data, e.g. for analysis, for interpretation, for correction
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01VGEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
    • G01V3/00Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation
    • G01V3/08Electric or magnetic prospecting or detecting; Measuring magnetic field characteristics of the earth, e.g. declination, deviation operating with magnetic or electric fields produced or modified by objects or geological structures or by detecting devices
    • G01V3/083Controlled source electromagnetic [CSEM] surveying
    • G01V2003/086Processing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/30Assessment of water resources

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  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Environmental & Geological Engineering (AREA)
  • Geology (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Geophysics (AREA)
  • Electromagnetism (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

The invention discloses a geological detection instrument, a geological detection method and a geological detection medium based on an unmanned aerial vehicle, wherein the detection instrument comprises an unmanned aerial vehicle, a signal receiving and transmitting detector and a signal processor; the signal receiving and transmitting detector is arranged on the unmanned aerial vehicle and comprises a signal transmitting coil used for transmitting a group of square wave current signals to the area to be detected, a receiving coil electrically connected with the signal transmitting coil and used for forming induced electromotive force according to magnetic field changes caused by receiving the square wave current signals in the area to be detected, and a signal collector electrically connected with the receiving coil and used for collecting the induced electromotive force; the signal processor is electrically connected with the signal collector and is used for receiving the signals collected by the signal collector and converting the received signals into geological data; therefore, the method solves the limitations of the traditional geophysical exploration method in terms of cost, efficiency, range, depth and the like, so as to improve the effect and efficiency of resource exploration and environment monitoring.

Description

Unmanned plane-based geological exploration instrument, method and medium
Technical Field
The invention relates to the technical field of geological exploration, in particular to a geological detection instrument, a geological detection method and a geological detection medium based on an unmanned plane.
Background
Traditional geophysical exploration methods such as seismic exploration, gravity measurement and the like have limitations in terms of coverage, depth of exploration, resolution and the like.
First, conventional geophysical prospecting methods often require large instrumentation and complex operational procedures, resulting in high costs, long times, and prospecting only for localized areas. This is not efficient in terms of resource exploration, environmental monitoring, etc. in a wide area. Second, conventional methods also have limitations in depth of investigation and resolution. For example, seismic exploration has a limited depth of investigation, while gravity measurement has a lower resolution, and deeper detailed information cannot be obtained.
Disclosure of Invention
The invention aims to overcome the defects of the background technology, and provides an unmanned plane-based geological exploration instrument, method and medium, which solve the limitations of the traditional geophysical exploration method in terms of cost, efficiency, range, depth and the like so as to improve the effects and efficiency of resource exploration and environment monitoring.
In a first aspect, there is provided an unmanned aerial vehicle-based geological exploration instrument, comprising:
an unmanned aerial vehicle;
The signal receiving and transmitting detector is arranged on the unmanned aerial vehicle and comprises a signal transmitting coil used for transmitting a group of square wave current signals to a region to be detected, a receiving coil electrically connected with the signal transmitting coil and used for forming induced electromotive force according to magnetic field changes caused by receiving the square wave current signals in the region to be detected, and a signal collector electrically connected with the receiving coil and used for collecting the induced electromotive force;
and the signal processor is electrically connected with the signal collector and is used for receiving the signals collected by the signal collector and converting the received signals into geological data.
In some embodiments, the signal transceiver detector further includes a multistage amplifier electrically connected to both the signal collector and the signal processor, where the multistage amplifier is configured to amplify the collected induced electromotive force.
In some embodiments, the signal transceiver detector further comprises a compensation coil, and the direction of the current signal passing through the compensation coil is opposite to the direction of the current signal passing through the signal transmitting coil.
In some embodiments, the signal transmitting coil, the receiving coil, and the compensating coil are in the same plane and concentric;
the receiving coil is arranged between the compensating coil and the signal transmitting coil, the radius of the compensating coil is smaller than that of the receiving coil, and the radius of the receiving coil is smaller than that of the signal transmitting coil.
In some embodiments, a connection cable connecting the signal transmitting coil, the receiving coil, and the compensation coil is further included.
In some embodiments, the signal collector is further configured to collect the signal of the induced electromotive force by high frequency sampling of 95-105 KHz.
In some embodiments, the signal transceiver detector further includes a memory electrically connected to the signal collector, where the memory is configured to store the signal collected by the signal collector.
In some embodiments, the signal processor is further configured to synthesize the signals amplified by each of the multiple stages of amplifiers, filter the synthesized signals, and convert the filtered signals into geological data.
In a second aspect, an aeronautical geological detection method is provided, which is applied to the unmanned aerial vehicle-based geological detection instrument, wherein the unmanned aerial vehicle-based geological detection instrument comprises an unmanned aerial vehicle, and a signal transmitting coil, a receiving coil, a signal collector, a multistage amplifier, a compensating coil and a signal processor which are arranged on the unmanned aerial vehicle, and the method comprises the following steps:
Transmitting a group of square wave current signals to a region to be detected by using a signal transmitting coil;
the receiving coil is used for receiving magnetic field changes caused by square wave current signals according to the area to be detected to form induced electromotive force;
the signal collector is used for collecting the induced electromotive force;
Amplifying the acquired induced electromotive force by using a multistage amplifier;
and receiving the signal amplified by the signal processor and converting the received signal into geological data.
The direction of the current signal which is introduced into the compensation coil is opposite to that of the current signal which is introduced into the signal transmitting coil.
In a third aspect, a computer readable storage medium is provided, on which a computer program is stored, characterized in that the computer program, when executed by a processor, implements an aeronautical geological detection method as described above.
In a fourth aspect, there is provided an electronic device comprising a storage medium, a processor and a computer program stored in the storage medium and executable on the processor, characterized in that the processor implements an aero-geological detection method as described above when running the computer program.
Compared with the prior art, the unmanned aerial vehicle is provided with the signal receiving and transmitting detector, a group of square wave current signals are transmitted to the ground through the signal receiving and transmitting detector in flight by utilizing the electromagnetic induction principle, the current signals are conducted to a region to be detected, induced electromotive force is formed on the receiving coil through the change of a magnetic field, the signal collector collects the induced electromotive force in real time to form a change curve, and then the signal collector carries out data processing to infer the electromagnetic characteristics of underground rock and soil, so that the structure and the components of the underground rock and soil are analyzed; therefore, the method solves the limitations of the traditional geophysical exploration method in terms of cost, efficiency, range, depth and the like, so as to improve the effect and efficiency of resource exploration and environment monitoring.
Drawings
FIG. 1 is a schematic diagram of an unmanned-vehicle-based geological exploration instrument and an area to be explored of the present invention;
Fig. 2 is a schematic diagram of a signal transmitting coil, a receiving coil, and a compensating coil of the present invention.
Detailed Description
Reference will now be made in detail to the present embodiments of the invention, examples of which are illustrated in the accompanying drawings. While the invention will be described in conjunction with the specific embodiments, it will be understood that they are not intended to limit the invention to the described embodiments. On the contrary, it is intended to cover alternatives, modifications, and equivalents as may be included within the spirit and scope of the invention as defined by the appended claims. It should be noted that the method steps described herein may be implemented by any functional block or arrangement of functions, and any functional block or arrangement of functions may be implemented as a physical entity or a logical entity, or a combination of both.
The present invention will be described in further detail below with reference to the drawings and detailed description for the purpose of enabling those skilled in the art to understand the invention better.
Note that: the examples to be described below are only one specific example, and not as limiting the embodiments of the present invention necessarily to the following specific steps, values, conditions, data, sequences, etc. Those skilled in the art can, upon reading the present specification, make and use the concepts of the invention to construct further embodiments not mentioned in the specification.
The embodiment of the invention provides a geological detection instrument based on an unmanned aerial vehicle, which comprises an unmanned aerial vehicle, a signal receiving and transmitting detector and a signal processor; the signal receiving and transmitting detector is arranged on the unmanned aerial vehicle and comprises a signal transmitting coil used for transmitting a group of square wave current signals to the area to be detected, a receiving coil electrically connected with the signal transmitting coil and used for forming induced electromotive force according to magnetic field changes caused by receiving the square wave current signals in the area to be detected, and a signal collector electrically connected with the receiving coil and used for collecting the induced electromotive force; the signal processor is electrically connected with the signal collector and is used for receiving the signals collected by the signal collector and converting the received signals into geological data.
Specifically, in this embodiment, referring to fig. 1, a signal transceiver probe is mounted on an unmanned aerial vehicle, and a set of square wave current signals are sent to the underground through the signal transceiver probe in flight by using the electromagnetic induction principle, the current signals will be conducted to a region to be detected, induced electromotive force is formed on a receiving coil through the change of a magnetic field, the signal collector collects the induced electromotive force in real time to form a change curve, and then data processing is performed through a signal processor to infer the electromagnetic characteristics of underground rock and soil, so that the structure and the components of the underground rock and soil are analyzed. Such geological exploration techniques as described above are described as aviation transient electromagnetic techniques.
Therefore, the aviation transient electromagnetic technology of the unmanned aerial vehicle-based geological detection instrument has the following beneficial effects:
1. high efficiency and high speed: the aviation transient electromagnetic technology can cover a large area through in-flight equipment, acquire a large amount of data in a short time and improve exploration efficiency.
2. Covering a large range: the aviation transient electromagnetic technology can realize continuous detection of a large-range area, is not limited by topography fluctuation and the like, and can acquire more comprehensive underground information.
3. Greater depth of investigation: the current signal (signal size is adjustable) emitted by aviation transient electromagnetic technology has a certain penetration depth, and can reach depths of hundreds of meters or even thousands of meters, thereby realizing detection of deeper underground structures.
4. High resolution: aviation transient electromagnetic technology can provide higher resolution so that finer subsurface structural information can be acquired.
In summary, the design background of the aviation transient electromagnetic technology is mainly used for solving the limitations of the traditional geophysical exploration method in terms of cost, efficiency, range, depth and the like, so as to improve the effects and efficiency of resource exploration and environment monitoring.
Optionally, the signal transceiver detector further includes a multistage amplifier electrically connected to the signal collector and the signal processor, where the multistage amplifier is used to amplify the collected induced electromotive force.
Specifically, in this embodiment, a multistage amplifier is used to increase the voltage acquisition range to 1 microvolts to 400 volts, and the minimum recognition accuracy is 1 microvolts, so that high-power emission during detection is realized, and the problem of weak received signals during detection is solved.
Optionally, the signal transceiver detector further includes a compensation coil, and a direction of a current signal flowing in the compensation coil is opposite to a direction of a current signal flowing in the signal transmitting coil.
Specifically, in this embodiment, the environmental interference is counteracted by adding a compensation coil. When current in the opposite direction to the signal transmitting coil is introduced into the compensating coil, the magnetic fluxes generated by the transmitting coil and the compensating coil are equal and opposite. At this time, the total magnetic flux acting on the receiving coil is zero, so that the primary field generated by the coil can be eliminated, and only the induced electromotive force fed back from the ground is received in the receiving coil, as shown in fig. 2.
Optionally, the signal transmitting coil, the receiving coil and the compensating coil are in the same plane and concentric;
the receiving coil is arranged between the compensating coil and the signal transmitting coil, the radius of the compensating coil is smaller than that of the receiving coil, and the radius of the receiving coil is smaller than that of the signal transmitting coil.
Optionally, the device further comprises a connecting cable for connecting the signal transmitting coil, the receiving coil and the compensating coil.
Optionally, the signal collector is further used for collecting the signal of the induced electromotive force through high-frequency sampling of 95-105 KHz. The signal is continuously read through high-frequency sampling of 95-105KHZ, so that the accuracy of data is ensured to a greater extent.
Optionally, the signal transceiver detector further includes a memory electrically connected to the signal collector, where the memory is configured to store the signal collected by the signal collector.
Specifically, in this embodiment, an external low-power memory is mounted on the signal collector, so that the data storage capacity is increased, the instrument performs faster during data storage, and the memory consumes less energy at the same time; because the external storage is adopted, the storage can be replaced immediately when the data is full, and the data can not be operated again until the data is exported.
Optionally, the signal processor is further configured to synthesize the signals amplified by each stage of the multi-stage amplifier, filter the synthesized signals, and convert the filtered signals into geological data.
Specifically, in this embodiment, the data in the memory is exported. And superposing the data of each stage of amplifier according to a fixed acquisition period, and synthesizing the data acquired by the plurality of amplifiers into continuous data in the whole range according to the range of the measured voltage of the amplifier. And processing the data by data filtering methods such as median, moving average, channel extraction and the like. And finally converting the processed data into geological data.
The invention belongs to an Aviation Transient Electromagnetic Method (ATEM), which is characterized in that an ungrounded loop is utilized to send step waves or other pulse currents to an underground geologic body (abnormal body in fig. 1), a primary field is generated around an underground changing electric field, the underground geologic body is induced to form a secondary field in an underground medium after power failure, a secondary field signal contains ground electric information of the underground geologic body, an attenuation signal of a secondary induction electromagnetic field changing along with time is measured during the period of breaking of the pulse current, and the electric conductivity of the underground geologic body and the spatial distribution condition of a target body can be analyzed from the measured abnormal electric field and magnetic field signals, namely, the attenuation signal of the secondary induction electromagnetic field changing along with time is obtained from converted geological data.
The prior methods are more for converting the received signals into geological data, and mainly comprise forward modeling of an aviation transient electromagnetic method, inversion of the aviation transient electromagnetic method and anisotropic inversion. The filtered signals are converted into resistivity data by adopting an aviation transient electromagnetic conductivity-depth imaging method, and the method comprises the following steps of:
There is some continuity due to the resistivity of the formation as a function of depth. Based on the characteristic, the resistivity of the next layer can be constrained according to the upper layer on the basis of the conductivity-depth imaging of the conventional table look-up method, and the corresponding apparent resistivity value of the layer can be found through a dichotomy. The method is specifically described in the university of Chengdu university's Shuoshi paper on aviation transient electromagnetic one-dimensional forward inversion and rapid imaging method research, chapter 4, aviation transient electromagnetic conductivity-depth imaging.
The embodiment of the invention also provides an aviation geological detection method which is applied to the geological detection instrument based on the unmanned aerial vehicle, wherein the geological detection instrument based on the unmanned aerial vehicle comprises an unmanned aerial vehicle, and a signal transmitting coil, a receiving coil, a signal collector, a multistage amplifier, a compensation coil and a signal processor which are arranged on the unmanned aerial vehicle, and comprises the following steps of:
s100, transmitting a group of square wave current signals to a region to be detected by using a signal transmitting coil;
s200, utilizing a receiving coil to receive magnetic field changes caused by square wave current signals according to a region to be detected so as to form induced electromotive force;
s300, collecting the induced electromotive force by using a signal collector;
s400, amplifying the acquired induced electromotive force by using a multi-stage amplifier;
S500, receiving the signal amplified by the signal processor and converting the received signal into geological data.
And S600, setting the direction of a current signal which is fed into the compensation coil to be opposite to the direction of a current signal which is fed into the signal transmitting coil.
The invention has the following beneficial effects:
1. High efficiency and high speed: the aviation transient electromagnetic technology can cover a large area through equipment in flight, acquire a large amount of data in a short time, improve exploration efficiency, realize unmanned in the acquisition process, and solve the detection requirement of an area which cannot be reached by people.
2. Covering a large range: the aviation transient electromagnetic technology can realize continuous detection of a large-range area, is not limited by topography fluctuation and the like, and can acquire more comprehensive underground information.
3. Greater depth of investigation: the aviation transient electromagnetic technology has a certain penetration depth, and can reach depths of hundreds of meters or even thousands of meters, so that detection of deeper underground structures is realized.
Increasing penetration depth: by increasing the magnitude of the emission current, the propagation depth of the emission current in the ground is deeper, and meanwhile, smaller interference signals can be suppressed.
4. High resolution: aviation transient electromagnetic technology can provide higher resolution so that finer subsurface structural information can be acquired.
Based on the same inventive concept, the embodiments of the present application also provide a computer-readable storage medium, on which a computer program is stored, which when being executed by a processor implements all or part of the method steps of the above method.
The present invention may be implemented by implementing all or part of the above-described method flow, or by instructing the relevant hardware by a computer program, which may be stored in a computer readable storage medium, and which when executed by a processor, may implement the steps of the above-described method embodiments. Wherein the computer program comprises computer program code, which may be in the form of source code, object code, executable files or in some intermediate form, etc. The computer readable medium may include: any entity or device capable of carrying computer program code, a recording medium, a U disk, a removable hard disk, a magnetic disk, an optical disk, a computer Memory, a Read-Only Memory (ROM), a random access Memory (RAM, random Access Memory), an electrical carrier signal, a telecommunications signal, a software distribution medium, and so forth. It should be noted that the content of the computer readable medium can be appropriately increased or decreased according to the requirements of the jurisdiction's jurisdiction and the patent practice, for example, in some jurisdictions, the computer readable medium does not include electrical carrier signals and telecommunication signals according to the jurisdiction and the patent practice.
Based on the same inventive concept, the embodiment of the application also provides an electronic device, which comprises a memory and a processor, wherein the memory stores a computer program running on the processor, and the processor executes the computer program to realize all or part of the method steps in the method.
The Processor may be a central processing unit (Central Processing Unit, CPU), other general purpose Processor, digital signal Processor (DIGITAL SIGNAL Processor, DSP), application SPECIFIC INTEGRA TED Circuit (ASIC), off-the-shelf Programmable gate array (Field-Programmable GATE ARRAY, FPGA) or other Programmable logic device, discrete gate or transistor logic device, discrete hardware components, or the like. A general purpose processor may be a microprocessor or the processor may be any conventional processor or the like, the processor being a control center of the computer device, and the various interfaces and lines connecting the various parts of the overall computer device.
The memory may be used to store computer programs and/or modules, and the processor implements various functions of the computer device by running or executing the computer programs and/or modules stored in the memory, and invoking data stored in the memory. The memory may mainly include a storage program area and a storage data area, wherein the storage program area may store an operating system, an application program required for at least one function (e.g., a sound playing function, an image playing function, etc.); the storage data area may store data (e.g., audio data, video data, etc.) created according to the use of the handset. In addition, the memory may include high-speed random access memory, and may also include non-volatile memory, such as a hard disk, memory, plug-in hard disk, smart memory card (SMART MEDIA CARD, SMC), secure Digital (SD) card, flash memory card (FLASH CARD), at least one disk storage device, flash memory device, or other volatile solid-state storage device.
It will be appreciated by those skilled in the art that embodiments of the present invention may be provided as a method, system, server, or computer program product. Accordingly, the present invention may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present invention may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, magnetic disk storage, optical storage, and the like) having computer-usable program code embodied therein.
The present invention is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), servers and computer program products according to embodiments of the invention. It will be understood that each flow and/or block of the flowchart illustrations and/or block diagrams, and combinations of flows and/or blocks in the flowchart illustrations and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
It will be apparent to those skilled in the art that various modifications and variations can be made to the present invention without departing from the spirit or scope of the invention. Thus, it is intended that the present invention also include such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.

Claims (10)

1. A geological exploration instrument based on unmanned aerial vehicle, characterized by comprising:
an unmanned aerial vehicle;
The signal receiving and transmitting detector is arranged on the unmanned aerial vehicle and comprises a signal transmitting coil used for transmitting a group of square wave current signals to a region to be detected, a receiving coil electrically connected with the signal transmitting coil and used for forming induced electromotive force according to magnetic field changes caused by receiving the square wave current signals in the region to be detected, and a signal collector electrically connected with the receiving coil and used for collecting the induced electromotive force;
and the signal processor is electrically connected with the signal collector and is used for receiving the signals collected by the signal collector and converting the received signals into geological data.
2. The unmanned aerial vehicle-based geological exploration instrument of claim 1, wherein said signal transceiver probe further comprises a multistage amplifier electrically connected to both said signal collector and signal processor, said multistage amplifier for amplifying the collected induced electromotive force.
3. The unmanned aerial vehicle-based geological exploration instrument of claim 1, wherein said signaling probe further comprises a compensation coil, said compensation coil having a current signal that is directed in a direction opposite to a current signal that is directed in said signal transmitting coil.
4. A drone-based geological exploration apparatus according to claim 3, wherein said signal transmitting coil, said receiving coil and said compensating coil are in the same plane and are concentric;
the receiving coil is arranged between the compensating coil and the signal transmitting coil, the radius of the compensating coil is smaller than that of the receiving coil, and the radius of the receiving coil is smaller than that of the signal transmitting coil.
5. The unmanned aerial vehicle-based geological exploration instrument of claim 3, further comprising a connection cable connecting said signal transmitting coil, said receiving coil and said compensating coil.
6. The unmanned aerial vehicle-based geological exploration apparatus of claim 1, wherein said signal collector is further configured to collect signals of induced electromotive force by high frequency sampling of 95-105 KHZ.
7. The unmanned aerial vehicle-based geological exploration instrument of claim 1, wherein said signal transceiver probe further comprises a memory electrically connected to said signal collector, said memory for storing signals collected by said signal collector.
8. The unmanned aerial vehicle-based geological exploration apparatus of claim 2, wherein the signal processor is further configured to synthesize the amplified signal from each of the plurality of stages of amplifiers, filter the synthesized signal, and convert the filtered signal into geological data.
9. An aviation geological detection method applied to the geological detection instrument based on the unmanned aerial vehicle as claimed in any one of claims 1 to 8, wherein the geological detection instrument based on the unmanned aerial vehicle comprises an unmanned aerial vehicle, and a signal transmitting coil, a receiving coil, a signal collector, a multistage amplifier, a compensating coil and a signal processor which are arranged on the unmanned aerial vehicle, and is characterized by comprising the following steps of:
Transmitting a group of square wave current signals to a region to be detected by using a signal transmitting coil;
the receiving coil is used for receiving magnetic field changes caused by square wave current signals according to the area to be detected to form induced electromotive force;
the signal collector is used for collecting the induced electromotive force;
Amplifying the acquired induced electromotive force by using a multistage amplifier;
receiving the signal amplified by the signal processor and converting the received signal into geological data;
the direction of the current signal which is introduced into the compensation coil is opposite to that of the current signal which is introduced into the signal transmitting coil.
10. A computer readable storage medium having stored thereon a computer program, which when executed by a processor implements the airborne geological detection method as claimed in claim 9.
CN202410181798.8A 2024-02-19 2024-02-19 Unmanned plane-based geological exploration instrument, method and medium Pending CN118169763A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202410181798.8A CN118169763A (en) 2024-02-19 2024-02-19 Unmanned plane-based geological exploration instrument, method and medium

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202410181798.8A CN118169763A (en) 2024-02-19 2024-02-19 Unmanned plane-based geological exploration instrument, method and medium

Publications (1)

Publication Number Publication Date
CN118169763A true CN118169763A (en) 2024-06-11

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