CN114063500B - Data synchronization testing device based on aeromagnetic superconducting full tensor magnetic gradient measurement and control system - Google Patents

Abstract

The embodiment of the application provides a synchronous testing arrangement of data based on magnetic superconducting full tensor magnetic gradient system of observing and controling of avionics, includes: the signal generator is configured to generate sine wave signals with preset frequency and transmit the sine wave signals to the NI9215 module and the full tensor magnetic data analog acquisition module; the NI9215 module is configured to trigger acquisition of sine wave signals based on the PPS signals to obtain first sine wave signals; the full-tensor magnetic data analog acquisition module is configured to amplify the sine wave signal based on the PPS signal to obtain a second sine wave signal; and the data acquisition and control system is configured to resample the second sine wave signal based on the PPS signal and a preset resampling rule to obtain a resampled second sine wave signal, and determine a phase difference between the first sine wave signal and the resampled second sine wave signal to realize phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

Description

Data synchronization test device based on aeromagnetic superconducting full tensor magnetic gradient measurement and control system

technical field

The application relates to the application field of superconductivity, and in particular, to a data synchronization test device based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system.

Background technique

The core sensor of the aeromagnetic superconducting full tensor gradient measurement and control system is the superconducting quantum interferometer, and the superconducting magnetic sensor composed of the superconducting quantum interferometer is the magnetic sensor with the highest sensitivity at present, which can measure tiny magnetic signals. However, since the airborne platform is moving, it is necessary to perform magnetic compensation through high-precision attitude projection to eliminate the interference introduced by the movement of the onboard platform. To eliminate these interferences, not only the measurement accuracy of position, attitude data and full tensor magnetic data is required as much as possible However, in the aeromagnetic superconducting full tensor gradient measurement and control system, due to the different data sources of the full tensor magnetic data and the position and attitude data , causing the full tensor magnetic data to be out of synchronization with the position and attitude data, and the synchronization accuracy is low when data synchronization is performed by the prior art.

SUMMARY OF THE INVENTION

The embodiment of the present application provides a data synchronization test device based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system, which can conveniently, quickly and effectively improve the synchronization accuracy of full tensor magnetic data and position and attitude data.

The technical solution of the present application is realized as follows:

The embodiment of the present application provides a data synchronization test device based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the device includes: a signal generator, an NI9215 module connected to the signal generator, and a full tensor magnetic A data simulation acquisition module, a data acquisition and control system connected with the NI9215 module and the full tensor magnetic data simulation acquisition module; wherein,

The signal generator is configured to generate a sine wave signal with a preset frequency and transmit it to the NI9215 module and the full tensor magnetic data analog acquisition module;

The NI9215 module is configured to trigger and collect the sine wave signal based on the second pulse PPS signal to obtain a first sine wave signal; and transmit the first sine wave signal to the data acquisition and control system; the NI9215 The module is a delay-free data acquisition card;

The full tensor magnetic data analog acquisition module is configured to amplify the sine wave signal based on the PPS signal to obtain a second sine wave signal; and transmit the second sine wave signal to the data acquisition and in the control system;

The data acquisition and control system is configured to resample the second sine wave signal based on the PPS signal and a preset resampling rule, obtain a resampled second sine wave signal, and determine the first sine wave signal. a phase difference between the sine wave signal and the resampled second sine wave signal, so as to achieve phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

In the above-mentioned data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the data acquisition and control system is connected with the inertial navigation system SPAN-CPT; wherein,

The data acquisition and control system is further configured to obtain the PPS signal from the SPAN-CPT when a preset time arrives; and transmit the PPS signal to the NI9215 module and the full tensor magnetic Data simulation acquisition module.

In the above data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the NI9215 module is further configured to trigger based on the PPS signal and collect the sine wave signal by using the first sampling frequency to obtain the the first sine wave signal; and transmit the first sine wave signal to the data acquisition and control system.

In the above-mentioned data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the full tensor magnetic data simulation acquisition module includes a readout circuit and a first data acquisition board; wherein,

The readout circuit is configured to perform integral amplification on the sine wave signal to obtain the integrally amplified sine wave signal, and transmit the integrally amplified sine wave signal to the first data acquisition board middle;

The first data acquisition board is configured to trigger based on the PPS signal and use the second sampling frequency to collect the integrated and amplified sine wave signal to obtain the second sine wave signal, and use the second sampling frequency to collect the second sine wave signal. Two sine wave signals are transmitted to the data acquisition and control system.

In the above-mentioned data synchronization test device based on aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the output port of the signal generator is respectively connected to the input port of the NI9215 module and the input of the readout circuit through a splitter port, the output port of the readout circuit is connected to the input port of the first data acquisition board, the output port of the first data acquisition board and the output port of the NI9215 module and the data acquisition and control system connected to the input port.

In the above-mentioned data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the data acquisition and control system is further configured to determine the first working parameter when the preset time arrives, and to An operating parameter is transmitted to the readout circuit, so that the readout circuit can integrate and amplify the sine wave signal based on the first operating parameter.

In the above data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the data acquisition and control system is further configured to extract the first phase of the first sine wave signal and the resampled the second phase of the second sine wave signal, the difference between the first phase and the second phase is determined as the phase difference, so as to realize the first sine wave signal and Phase synchronization between the second sine wave signals.

In the above data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the first sampling frequency is 1000 Hz.

In the above data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the second sampling frequency is 1000 Hz.

In the above data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the first data acquisition board is NI9234.

The embodiment of the present application provides a data synchronization test device based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the device includes: a signal generator, an NI9215 module connected to the signal generator, and a full tensor magnetic data simulation The acquisition module is a data acquisition and control system connected with the NI9215 module and the full tensor magnetic data analog acquisition module; the signal generator is configured to generate a sine wave signal with a preset frequency and transmit it to the NI9215 module and the full tensor magnetic data acquisition module; In the data analog acquisition module; the NI9215 module is configured to trigger the acquisition of the sine wave signal based on the second pulse PPS signal to obtain the first sine wave signal; and transmit the first sine wave signal to the data acquisition and control system; the NI9215 module has no delay Data acquisition card; full tensor magnetic data analog acquisition module, configured to amplify the sine wave signal based on the PPS signal to obtain the second sine wave signal; and transmit the second sine wave signal to the data acquisition and control system; data acquisition and the control system, configured to resample the second sine wave signal based on the PPS signal and the preset resampling rule, obtain a second sine wave signal after resample, and determine the first sine wave signal and the second sine wave signal after resampling The phase difference between the sine wave signals is used to realize the phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference; using the above implementation scheme, after the sine wave signal is generated, the sine wave signal is respectively input in advance. Set the NI9215 module and the full tensor magnetic data simulation acquisition module to simulate the process of collecting position, attitude data and resampled full tensor magnetic data in the actual situation, and then obtain the NI9215 module and the full tensor magnetic data simulation acquisition After the first sine wave signal and the second sine wave signal output by the module, the phase difference between the two is calculated, and then the phase difference is used to compensate the second sine wave signal, that is, the data synchronization between the two is realized. By using this phase difference to compensate the resampled full tensor magnetic data, the purpose of improving the data synchronization accuracy of the position, attitude data and the resampled full tensor magnetic data can be achieved, so that the final data synchronization accuracy can reach 5 microseconds within.

Description of drawings

1 is a schematic diagram of a connection of a data synchronization testing device 1 based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system provided by an embodiment of the application;

2 is a schematic diagram 2 of a connection of a data synchronization test device 1 based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system provided by an embodiment of the application;

FIG. 3 is a schematic diagram of an exemplary signal acquisition result provided by an embodiment of the present application;

FIG. 4 is a schematic diagram of an exemplary test result provided by an embodiment of the present application.

Detailed ways

Aeronautical superconducting full tensor magnetic gradient data acquisition and control system not only needs to collect full tensor magnetic data, but also needs real-time position and attitude data corresponding to full tensor magnetic data, and the higher the synchronization, the better. The attitude data is used to effectively eliminate the interference introduced by the full tensor magnetic data in the motion state, and then the spatial distribution information of the measured area can be obtained by corresponding the full tensor magnetic data after eliminating the interference with the position information. Therefore, the measurement accuracy of the position and attitude data and the synchronization with the full tensor magnetic data determine the data quality of the aviation superconducting full tensor magnetic gradient data acquisition and control system. Different data sources cause the full tensor magnetic data to be out of sync with the position and attitude data.

The data synchronization of the position, attitude data and the full tensor magnetic data can be obtained by resampling the full tensor magnetic data. Since the position and attitude data are directly connected to the data acquisition and control system by the inertial navigation system SPAN-CPT, the data acquisition and The control system is directly obtained from SPAN-CPT, so the delay of the position and attitude data can be ignored at this time, but before resampling the full tensor magnetic data, the full tensor magnetic The data is integrated and amplified, and the analog-to-digital conversion of the full tensor magnetic data is required. At this time, the full tensor magnetic data will be delayed, resulting in a certain amount of resampled full tensor magnetic data compared with the position and attitude data. Therefore, there is a certain time delay between the resampled full tensor magnetic data and the position and attitude data.

Based on the above problems, this application proposes a data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system, which is used to test the full tensor magnetic data and The time delay will be generated in the process of sampling the position and attitude data, and then the resampling parameters of the full tensor magnetic data will be adjusted through this time delay, and the synchronization accuracy of the full tensor magnetic data and the position and attitude data will be improved.

It should be understood that the specific embodiments described herein are merely illustrative of the present application. It is not intended to limit this application.

The embodiment of the present application provides a data synchronization test device 1 based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system. The first connection diagram of the data synchronization test device 1, as shown in Figure 1, the data synchronization test device 1 based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system may include:

The signal generator 10, the NI9215 module 11 and the full tensor magnetic data analog acquisition module 12 connected with the signal generator, the data acquisition and control system 13 connected with the NI9215 module and the full tensor magnetic data analog acquisition module; wherein,

A signal generator, configured to generate a sine wave signal with a preset frequency and transmit it to the NI9215 module and the full tensor magnetic data analog acquisition module;

The NI9215 module is configured to trigger the acquisition of the sine wave signal based on the second pulse PPS signal to obtain the first sine wave signal; and transmit the first sine wave signal to the data acquisition and control system; the NI9215 module is a delay-free data acquisition card;

The full tensor magnetic data analog acquisition module is configured to amplify the sine wave signal based on the PPS signal to obtain the second sine wave signal; and transmit the second sine wave signal to the data acquisition and control system;

The data acquisition and control system is configured to resample the second sine wave signal based on the PPS signal and the preset resampling rule, obtain the resampled second sine wave signal, and determine the first sine wave signal and the resampled sine wave signal. The phase difference between the second sine wave signals to achieve phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

The data synchronization testing device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system provided by the embodiment of the present application is suitable for testing the full tensor magnetic data and position, In the process of sampling the attitude data, the time delay between the full tensor magnetic data and the position and attitude data is used to compensate the full tensor magnetic data after resampling through this delay time.

It should be noted that, in the embodiment of the present application, the preset frequency is 50 Hz, and the specific preset frequency can be specified according to the actual situation, which is not limited in the embodiment of the present application.

It should be noted that the sine wave signal generated by the signal generator may not be required to have zero phase, nor is it required to be triggered by the PPS signal.

It should be noted that the NI9215 module and the full tensor magnetic data simulation acquisition module are respectively used to simulate the process of collecting position and attitude data and the process of collecting resampled full tensor magnetic data in actual situations.

In the embodiment of the present application, the data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system is connected with the inertial navigation system SPAN-CPT through the data acquisition and control system; wherein, the data acquisition and control system is also configured In order to obtain the PPS signal from the SPAN-CPT when the preset time arrives; and transmit the PPS signal to the NI9215 module and the full tensor magnetic data analog acquisition module.

It should be noted that after the SPAN-CPT converges, the Pulse Per Second (PPS) signal of the Global Positioning System (GPS) is reliable. After the CPT converges, the PPS signal is obtained from the SPAN-CPT.

In the embodiment of the present application, the NI9215 module is further configured to be triggered based on the PPS signal, use the first sampling frequency to collect the sine wave signal to obtain the first sine wave signal, and transmit the first sine wave signal to the data acquisition and control system.

It should be noted that since the data acquisition and control system is connected to SPAN-CPT, in actual situations, the data acquisition and control system can directly collect the pose data in SPAN-CPT, that is, position and attitude data, and the delay can be ignored. Regardless, this application uses the NI9215 card to simulate the process of collecting pose data in the actual situation. Since the NI9215 card is a non-delay successive approximation register (Successive Approximation Register, SAR) data acquisition board, it contains 4 synchronization Sampling the analog input channel has no sampling delay but has a microsecond-level conversion time. This conversion time affects the sampling frequency and does not generate sampling delay. Therefore, it can be used to simulate the process of collecting pose data in actual situations.

In the embodiment of the present application, the NI9215 uses the first sampling frequency of 1000 Hz to collect the sine wave signal.

It should be noted that, in the embodiment of the present application, the NI9215 card without delay is used to collect the sine wave signal to simulate the process of collecting the pose data in the SPAN-CPT by the data acquisition and control system in the actual situation.

In the embodiment of the present application, the full tensor magnetic data analog acquisition module includes a readout circuit and a first data acquisition board; wherein, the readout circuit is configured to perform integral amplification on a sine wave signal to obtain an integrally amplified sine wave signal, and transmit the integrated and amplified sine wave signal to the first data acquisition board; the first data acquisition board is configured to trigger based on the PPS signal and use the second sampling frequency to collect the integrated and amplified sine wave signal. , obtain the second sine wave signal, and transmit the second sine wave signal to the data acquisition and control system.

It should be noted that, in the actual situation, the resampling of the full tensor magnetic data is realized by the host computer program of the data acquisition and control system. Therefore, in the simulation, it is necessary to make the sine wave signal generated by the signal generator. After the readout circuit and the first data acquisition board, and after the second sine wave signal is obtained, it is sent to the data acquisition and control system. The phase of the sampled second sine wave signal is compared with the first sine wave.

It should be noted that the first data acquisition board may be a data acquisition and control system acquisition board, as long as it is a data acquisition card used in the process of resampling the full tensor magnetic data. In this embodiment of the present application, The first data acquisition board is NI9234, and the specific first data acquisition board may be determined according to the actual situation, which is not limited in this embodiment of the present application.

It should be noted that, in this embodiment of the present application, the second sampling frequency is 1000 Hz.

It should be noted that, in practice, when the full tensor magnetic data is resampled using the resampling rule, the full tensor magnetic data is time stamped based on the PPS signal in SPAN-CPT. Therefore, in the simulation , it is also necessary to trigger the acquisition of full tensor magnetic data based on the PPS signal in SPAN-CPT, and resample the data after acquisition.

In the embodiment of the present application, the output port of the signal generator is connected to the input port of the NI9215 module and the input port of the readout circuit respectively through the splitter, and the output port of the readout circuit is connected to the input port of the first data acquisition board, the first The output port of a data acquisition board and the output port of the NI9215 module are connected with the input port of the data acquisition and control system.

In the embodiment of the present application, the data acquisition and control system is further configured to determine the first working parameter when the preset time arrives, and transmit the first working parameter to the amplifying circuit, so that the amplifying circuit can use the first working parameter based on the first working parameter. Amplify the sine wave signal.

It should be noted that the process of determining the first working parameter is the preparatory work before the start of the test, and the arrival of the preset time can be understood as determining the first working parameter of the readout circuit after the SPAN-CPT converges and before the start of the test. The first operating parameter is transmitted to the amplifying circuit, so that the readout circuit is in a normal working state.

In the embodiment of the present application, the data acquisition and control system is further configured to extract the first phase of the first sine wave signal and the second phase of the resampled second sine wave signal, and combine the first phase and the second phase The difference therebetween is determined as a phase difference to achieve phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

It should be noted that, after the data acquisition and control system obtains the first sine wave signal and the resampled second sine wave signal, the first phase of the first sine wave signal is extracted, and the second phase of the second sine wave signal is extracted. , determine the phase difference between the first sine wave signal and the second sine wave signal based on the first phase and the second phase, and then use this phase difference to compensate the resampled second sine wave signal to achieve the first sine wave signal and the phase synchronization between the resampled second sine wave signal, and then, in practice, after obtaining the position and attitude data and collecting the resampled full tensor magnetic data, this phase difference is used to directly compensate the resampling After the full tensor magnetic data, the synchronization accuracy of the two can be further improved.

Exemplarily, the embodiment of the present application provides a schematic diagram of the connection of the data synchronization test device 1 based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system. The data synchronization test device of the gradient measurement and control system includes: a signal generator, NI9215, a readout circuit, a first data acquisition board and a data acquisition and control system, wherein the output end of the signal generator is respectively connected with the input of the NI9215 and the readout circuit. The output end of the readout circuit is connected to the input end of the first data acquisition board. At the same time, the NI9215 and the output end of the first data acquisition board are connected to the data acquisition and control system, and the inertial navigation system SPAN-CPT It is also connected to the data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system by connecting the data acquisition and control system.

Based on the data synchronization test device based on the aeromagnetic superconducting full tensor magnetic gradient measurement and control system in Fig. 2, and the first data acquisition board selects NI9234, the collected first sine wave signal and second sine wave signal such as As shown in FIG. 3 , FIG. 3 is a schematic diagram of an exemplary signal acquisition result given by an embodiment of the application. The upper half of FIG. 3 represents the second sine wave signal, and the lower half represents the first sine wave signal. The phases of the first sine wave signal and the second sine wave signal are extracted and made difference, and the phase difference between the two can be obtained, as shown in FIG. 4 is the synchronization accuracy of the synchronization data after compensation. In Figure 4, the vertical axis is the conversion time after the phase difference is calculated, in nanoseconds, and the horizontal axis is the number of data points. The test results show that the average delay is -75.86ns, and the maximum delay is -75.86ns. 1483ns, the minimum delay is -1853ns, and the delay fluctuation is 3337ns. Based on Figure 4, it can be seen that the delay fluctuation is less than 5 microseconds, indicating that this device can test the synchronization accuracy of similar systems.

The embodiment of the present application provides a data synchronization test device based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system, the device includes: a signal generator, an NI9215 module connected to the signal generator, and a full tensor magnetic data simulation The acquisition module is a data acquisition and control system connected with the NI9215 module and the full tensor magnetic data analog acquisition module; the signal generator is configured to generate a sine wave signal with a preset frequency and transmit it to the NI9215 module and the full tensor magnetic data acquisition module; In the data analog acquisition module; the NI9215 module is configured to trigger the acquisition of the sine wave signal based on the second pulse PPS signal to obtain the first sine wave signal; and transmit the first sine wave signal to the data acquisition and control system; the NI9215 module has no delay Data acquisition card; full tensor magnetic data analog acquisition module, configured to amplify the sine wave signal based on the PPS signal to obtain the second sine wave signal; and transmit the second sine wave signal to the data acquisition and control system; data acquisition and the control system, configured to resample the second sine wave signal based on the PPS signal and the preset resampling rule, obtain a second sine wave signal after resample, and determine the first sine wave signal and the second sine wave signal after resampling The phase difference between the sine wave signals is used to realize the phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference; using the above implementation scheme, after the sine wave signal is generated, the sine wave signal is respectively input in advance. Set the NI9215 module and the full tensor magnetic data simulation acquisition module to simulate the process of collecting position, attitude data and resampled full tensor magnetic data in the actual situation, and then obtain the NI9215 module and the full tensor magnetic data simulation acquisition After the first sine wave signal and the second sine wave signal output by the module, the phase difference between the two is calculated, and then the phase difference is used to compensate the second sine wave signal, that is, the data synchronization between the two is realized. By using this phase difference to compensate the resampled full tensor magnetic data, the purpose of improving the data synchronization accuracy of the position, attitude data and the resampled full tensor magnetic data can be achieved, so that the final data synchronization accuracy can reach 5 microseconds within.

As will be appreciated by those skilled in the art, the embodiments of the present application may be provided as a method, a system, or a computer program product. Accordingly, the application may take the form of a hardware embodiment, a software embodiment, or an embodiment combining software and hardware aspects. Furthermore, the present application may take the form of a computer program product embodied on one or more computer-usable storage media having computer-usable program code embodied therein, including but not limited to disk storage, optical storage, and the like.

The present application is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the present application. It will be understood that each flow and/or block in 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 the processor of a general purpose computer, special purpose computer, embedded processor or other programmable data processing device to produce a machine such that the instructions executed by the processor of the computer or other programmable data processing device produce Means for implementing the functions specified in a flow or flow of a flowchart and/or a block or blocks of a block diagram.

These computer program instructions may also be stored in a computer-readable memory capable of directing a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory result in an article of manufacture comprising instruction means, the instructions The apparatus implements the functions specified in the flow or flow of the flowcharts and/or the block or blocks of the block diagrams.

These computer program instructions can also be loaded on a computer or other programmable data processing device to cause a series of operational steps to be performed on the computer or other programmable device to produce a computer-implemented process such that The instructions provide steps for implementing the functions specified in the flow or blocks of the flowcharts and/or the block or blocks of the block diagrams.

The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention.

Claims (10)

1. The utility model provides a synchronous testing arrangement of data based on magnetic superconducting full tensor magnetic gradient system of observing and controling which characterized in that, the device includes: the system comprises a signal generator, an NI9215 module, a full tensor magnetic data simulation acquisition module and a data acquisition and control system, wherein the NI9215 module and the full tensor magnetic data simulation acquisition module are connected with the signal generator; wherein,

the signal generator is configured to generate sine wave signals with preset frequency and transmit the sine wave signals to the NI9215 module and the full-tensor magnetic data analog acquisition module;

the NI9215 module is configured to trigger and collect the sine wave signal based on a pulse per second PPS signal to obtain a first sine wave signal; transmitting the first sine wave signal to the data acquisition and control system; the NI9215 module is a non-delay data acquisition card;

the full-tensor magnetic data analog acquisition module is configured to amplify the sine wave signal based on the PPS signal to obtain a second sine wave signal; transmitting the second sine wave signal to the data acquisition and control system;

the data acquisition and control system is configured to resample the second sine wave signal based on the PPS signal and a preset resampling rule to obtain a resampled second sine wave signal, and determine a phase difference between the first sine wave signal and the resampled second sine wave signal to realize phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

2. The device of claim 1, wherein the data acquisition and control system is connected with an inertial navigation system SPAN-CPT; wherein,

the data acquisition and control system is further configured to acquire the PPS signal from the SPAN-CPT when a preset time is reached; and transmitting the PPS signal to the NI9215 module and the full-tensor magnetic data analog acquisition module.

3. The apparatus of claim 1, wherein the NI9215 module is further configured to acquire the sine wave signal with a first sampling frequency based on the PPS signal trigger, resulting in the first sine wave signal; and transmitting the first sine wave signal to the data acquisition and control system.

4. The device of claim 3, wherein the full tensor magnetic data analog acquisition module comprises a readout circuit and a first data acquisition board card; wherein,

the reading circuit is configured to perform integral amplification on the sine wave signal to obtain an integral amplified sine wave signal, and transmit the integral amplified sine wave signal to the first data acquisition board card;

the first data acquisition board card is configured to acquire the sine wave signal subjected to integral amplification by using a second sampling frequency based on the PPS signal trigger to obtain a second sine wave signal, and transmit the second sine wave signal to the data acquisition and control system.

5. The device of claim 4, wherein an output port of the signal generator is connected to an input port of the NI9215 module and an input port of the readout circuit through a splitter, an output port of the readout circuit is connected to an input port of the first data acquisition board, and an output port of the first data acquisition board and an output port of the NI9215 module are connected to an input port of the data acquisition and control system.

6. The apparatus of claim 4,

the data acquisition and control system is further configured to determine a first working parameter when a preset time is reached, and transmit the first working parameter to the readout circuit, so that the readout circuit performs integral amplification on the sine wave signal based on the first working parameter.

7. The apparatus of claim 1,

the data acquisition and control system is further configured to extract a first phase of the first sine wave signal and a second phase of the resampled second sine wave signal and determine a difference between the first phase and the second phase as the phase difference to achieve phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

8. The apparatus of claim 3, wherein the first sampling frequency is 1000 hertz.

9. The apparatus of claim 4, wherein the second sampling frequency is 1000 hertz.

10. The apparatus of claim 4, wherein the first data acquisition board is NI 9234.

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