Fault Diagnosis for Satellite Attitude System by Simplified Filter Scheme

被引：0
|
作者：
Li L.-L. [1 ,2 ,3 ]
Niu R. [2 ,3 ]
Shao Z.-J. [2 ,3 ]
Shen Y. [1 ]
机构：
[1] School of Astronautics, Harbin Institute of Technology, Harbin
[2] Shanghai Institute of Spaceflight Control Technology, Shanghai
[3] Shanghai Key Laboratory of Aerospace Intelligent Control Techology, Shanghai
来源：
Yuhang Xuebao/Journal of Astronautics | 2019年 / 40卷 / 07期
关键词：
Attitude determination system; Fault diagnosis; Kalman filter;
D O I：
10.3873/j.issn.1000-1328.2019.07.006
中图分类号：
学科分类号：
摘要：
Considering the fact that the computation resources of an on-orbit computer are limited, this paper proposes a fault detection and isolation method based on a Kalman filter to reduce the computation load of the fault diagnosis for a satellite attitude determination system. In the proposed method, a novel additive Kalman filter is designed based on the attitude kinematics, and then a sensor fault diagnosis method is presented using the simplified filter scheme by integrating the Kalman filter with the simplified observer scheme (SOS). The proposed fault diagnosis method not only can detect and isolate the gyro fault, but also can diagnose the fault of the star sensor. In this method, only one filter is used to achieve the fault detection and isolation. Moreover, it is easy for computation and hence is useful in on-orbit implementation. The proposed method is verified by an attitude determination system consisting of a tri-orthogonal-one-slant gyro component and a star sensor. The simulation results show the effectiveness of the proposed method. © 2019, Editorial Dept. of JA. All right reserved.
引用
收藏
页码：776 / 784
页数：8
相关论文
共 19 条
  • [1] Li Z., Liu G., Zhang R., Et al., Fault detection, identification and reconstruction for gyroscope in satellite based on independent component analysis, Acta Astronautica, 68, 7-8, pp. 1015-1023, (2011)
  • [2] Tafazoli M., A study of on-orbit spacecraft failures, Acta Astronautica, 64, 2-3, pp. 195-205, (2009)
  • [3] Chiang L.H., Russel E.L., Braatz R.D., Fault Detection and Diagnosis in Industrial Systems, (2002)
  • [4] Xing Y., Wu H.-X., Wang X.-L., Et al., Survey of fault diagnosis and fault-tolerant control technology for spacecraft, Journal of Astronautics, 24, 3, pp. 221-226, (2003)
  • [5] Jiang L.-X., Li H.-W., Yang G.-Q., Et al., A survey of spacecraft autonomous fault diagnosis research, Journal of Astronautics, 30, 4, pp. 1320-1326, (2009)
  • [6] Song Z.-Y., The survey of launch vehicle long distance fault diagnosis technique, Journal of Astronautics, 37, 2, pp. 135-144, (2016)
  • [7] Venkateswaran N., Siva M.S., Goel P.S., Analytical redundancy based fault detection of gyroscopes in spacecraft applications, Acta Astronautica, 50, 9, pp. 535-545, (2002)
  • [8] Shen Y., Wang Z., Zhang X., Fault diagnosis and fault-tolerant control for sampled-data attitude control systems: an indirect approach, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 228, 7, pp. 1047-1157, (2014)
  • [9] Jia Q., Chen W., Zhang Y., Et al., Integrated design of fault reconstruction and fault-tolerant control against actuator faults using learning observers, International Journal of Systems Science, 47, 16, pp. 3749-3761, (2016)
  • [10] Cheng Y., Wang R., Xu M., Et al., Simultaneous state and actuator fault estimation for satellite attitude control systems, Chinese Journal of Aeronautics, 29, 3, pp. 714-721, (2016)
12