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

A measurement and control system and data synchronization technology, applied in the field of superconducting applications, can solve problems such as low synchronization accuracy, asynchronous full tensor magnetic data and position and attitude data, etc.

Active Publication Date: 2022-02-18
AEROSPACE INFORMATION RES INST CAS
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Problems solved by technology

However, since the aviation carrying 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 carrying platform. Eliminating these interferences not only requires the measurement accuracy of position, attitude data and full tensor magnetic data to be as accurate as possible High, and require position, attitude data and full tensor magnetic data must maintain a high degree of synchronization, but in the aeromagnetic superconducting full tensor gradient measurement and control system, due to the different data sources of full tensor magnetic data and position, attitude data , resulting in out-of-synchronization of full tensor magnetic data and position and attitude data, and low synchronization accuracy when data synchronization is performed through existing technologies

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

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Embodiment Construction

[0027] The 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 the 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 moving state, and then the full tensor magnetic data after the interference is eliminated corresponds to the position information to obtain the spatial distribution information of the measured area. 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 aeronautical superconducting full tensor magnetic gradient data acquisition and control system. The data sources are different, resulting in asynchronous full tensor magnetic data and position and attitud...

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Abstract

The embodiment of the invention provides a data synchronization test device based on an aeromagnetic superconducting full-tensor magnetic gradient measurement and control system, and the device comprises a signal generator which is configured to generate a sine wave signal with a preset frequency and transmit the sine wave signal to an NI9215 module and a full-tensor magnetic data simulation collection module; an NI9215 module which is configured to trigger and collect a sine wave signal based on a pulse per second (PPS) signal to obtain a first sine wave signal; a full-tensor magnetic data simulation acquisition module which is configured to amplify the sine wave signal based on the PPS signal to obtain a second sine wave signal; and a data acquisition and control system which is configured to re-sample the second sine wave signal based on the PPS signal and a preset re-sampling rule to obtain a re-sampled second sine wave signal, determine a phase difference between the first sine wave signal and the re-sampled second sine wave signal, and realize phase synchronization between the first sine wave signal and the second sine wave signal based on the phase difference.

Description

technical field [0001] The present application relates to the field of superconducting applications, in particular to a data synchronization testing device based on an aeromagnetic superconducting full tensor magnetic gradient measurement and control system. Background technique [0002] The core sensor of the aeromagnetic superconducting full tensor gradient measurement and control system is a superconducting quantum interferometer, and a superconducting magnetic sensor composed of a superconducting quantum interferometer is currently the most sensitive magnetic sensor, which can measure tiny magnetic signals. However, since the aviation carrying 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 carrying platform. Eliminating these interferences not only requires the measurement accuracy of position, attitude data and full tensor magnetic data to be a...

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Application Information

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IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/25257
Inventor 刘建英郭子祺乔彦超秦静欣侯瑞东
Owner AEROSPACE INFORMATION RES INST CAS
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