Volume 12 Issue 3
Jun.  2019
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CHAI Guo-zhi, HUANG Liang, QIAO Liang, ZHANG Guan-mao. Effect of the on-board residual magnetism on inertial sensors[J]. Chinese Optics, 2019, 12(3): 515-525. doi: 10.3788/CO.20191203.0515
Citation: CHAI Guo-zhi, HUANG Liang, QIAO Liang, ZHANG Guan-mao. Effect of the on-board residual magnetism on inertial sensors[J]. Chinese Optics, 2019, 12(3): 515-525. doi: 10.3788/CO.20191203.0515

Effect of the on-board residual magnetism on inertial sensors

doi: 10.3788/CO.20191203.0515

the Fundamental Research Funds for the Central Universities lzujbky-2018-k11

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  • Corresponding author: CHAI Guo-zhi, E-mail:chaigzh@lzu.edu.cn
  • Received Date: 20 Apr 2019
  • Rev Recd Date: 07 May 2019
  • Publish Date: 01 Jun 2019
  • The requirement of space gravitational wave detection on residual acceleration is extremely high(10-15 ms-2Hz-1/2), and the environmental magnetic field will cause magnetic force and Lorentz force. To ensure the accurately detection of gravitational wave, the environmental magnetic field and its gradient must be controlled within a low range. In this paper, we mainly research the effect of the on-board residual magnetism on internal sensors. Then, the relationship between residual magnetism and acceleration is explored from the aspects of interstellar magnetic field, residual magnetism of satellite components and time-varying magnetic field detection. Moreover, the simulation and detection of magnetic field are discussed. The results show that the remanence magnetic field can be reduced by optimizing the location and the orientation of the magnetic source. It is necessary to control magnetic field noise by real-time monitoring of interstellar magnetic field and time-varying magnetic field by adopting weak magnetic detection device for obtaining high-precision gravitational wave detection data. It can be concluded that it's necessary to analyze the influence of on-board residual magnetism on the inertial sensors, and the magnetic field evaluation schemes and weak magnetic detection methods for satellite platform should be developed.


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