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A Detection Method for the Random Noise Failure of Mems Gyros on Orbit

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Russian Physics Journal Aims and scope

The extended Kalman filter and parity vector method are combined to optimize the gyros fault diagnosis model, compensate the constant drift, and increase the time window to improve the fault decision function. The improved model retains the ability to detect the abnormal drift faults and it can effectively detect the abnormal noise faults to isolate the fault type for the application of MEMS on orbit. The algorithm model of real satellite attitude control system is used to make the simulation verification. The results show that the system can effectively detect and isolate the fault type in a short time.

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References

  1. W. Wang, Infrared Laser Eng., 45, No. 3, 1–6 (2016).

    Google Scholar 

  2. H. R. Petersen, R. Holm, H. E. Mathisen, et al., 33th Annual AIAA/USU Conference on Small Satellites, SSC19–VII–01 (2019).

  3. Y. Xing and C. L. Wei, J. Astronautics, 24, No. 4, 410–417 (2003).

    Google Scholar 

  4. S. Qian, P. K. Li, and S. F. Zhang, J. Astronautics, 30, No. 2, 585–590 (2009).

    Google Scholar 

  5. L. L. Li, R. Niu, and Z. J. Shao, J. Astronautics, 40, No. 7, 776–784 (2019).

    Google Scholar 

  6. Y. N. Wang, Z. J. Ren, and J. Yan, J. Spacecraft TT & C, No.1, 83–86 (2015).

  7. S. Yoon, S. Kim, J. Bae, et al., Control Eng Pract., 19. No. 2, 158–173 (2011).

    Article  Google Scholar 

  8. C. B. Li and Z. L. Zhang, Aerospace Control., 34, No. 2, 86–90 (2016).

    Google Scholar 

  9. B. H. Du, Z. Y. Shi, J. L. Song, et al., Micromachines, 10, No. 5, 278 (2019).

    Article  Google Scholar 

  10. K. Kaladhar, E. Komuraiah, and K. M. Reddy, Appl. Math. Nonlinear Sci., 4, No. 2, 475–488 (2019).

    Article  MathSciNet  Google Scholar 

  11. P. Zhou and Q. Fan, J. Zhu, Appl. Math. Nonlinear Sci., 5, No. 1, 25–34 (2020).

    Article  Google Scholar 

  12. T. Zhang, F. F. Wang, and W. X. Fu, Appl. Sci., 8, No. 6, 865 (2018).

    Article  Google Scholar 

  13. C. Xu, S. Y. Zhao, and F. Liu, Neurocomputing, 349, 156–163 (2019).

    Article  Google Scholar 

  14. J. Z. Lu, C. X. Zhang, and T. Y. Yan, J. Astronautics, 30, No. 3, 982–987 (2009).

    Google Scholar 

  15. D. Hu and Y. F. Dong, Chin. J. Space Sci., 31, No. 2, 229–235 (2011).

    Google Scholar 

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Authors and Affiliations

  1. School of Automation, Northwestern Polytechnical University, Xi’an, China

    Xia Mu & Sihai Li

  2. Beijing Commsat Technology Development Co., Ltd, Beijing, China

    Zhao Wang & Zhuoran Yao

  3. School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing, China

    Zhuoran Yao

Authors
  1. Xia Mu
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  2. Sihai Li
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  3. Zhao Wang
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  4. Zhuoran Yao
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Corresponding author

Correspondence to Xia Mu.

Additional information

Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Fizika, No. 10, pp. 66–78, October, 2021.

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Mu, X., Li, S., Wang, Z. et al. A Detection Method for the Random Noise Failure of Mems Gyros on Orbit. Russ Phys J 64, 1857–1871 (2022). https://doi.org/10.1007/s11182-022-02526-3

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  • DOI: https://doi.org/10.1007/s11182-022-02526-3

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