Neural network-based fault diagnosis for spacecraft with single-gimbal control moment gyros

被引:0
|
作者
Yuandong LI [1 ,2 ]
Qinglei HU [1 ,2 ]
Xiaodong SHAO [3 ]
机构
[1] School of Automation Science and Electrical Engineering, Beihang University
[2] Beihang Hangzhou Innovation Institute Yuhang
[3] School of Aeronautic Science and Engineering, Beihang University
基金
中国博士后科学基金; 中国国家自然科学基金; 北京市自然科学基金;
关键词
D O I
暂无
中图分类号
TP183 [人工神经网络与计算]; V467 [航天器的维护与修理];
学科分类号
081104 ; 0812 ; 082503 ; 0835 ; 1405 ;
摘要
This paper proposes a neural network-based fault diagnosis scheme to address the problem of fault isolation and estimation for the Single-Gimbal Control Moment Gyroscopes(SGCMGs) of spacecraft in a periodic orbit. To this end, a disturbance observer based on neural network is developed for active anti-disturbance, so as to improve the accuracy of fault diagnosis.The periodic disturbance on orbit can be decoupled with fault by resorting to the fitting and memory ability of neural network. Subsequently, the fault diagnosis scheme is established based on the idea of information fusion. The data of spacecraft attitude and gimbals position are combined to implement fault isolation and estimation based on adaptive estimator and neural network. Then,an adaptive sliding mode controller incorporating the disturbance and fault estimation results is designed to achieve active fault-tolerant control. In addition, the paper gives the proof of the stability of the proposed schemes, and the simulation results show that the proposed scheme achieves better diagnosis and control results than compared algorithm.
引用
收藏
页码:261 / 273
页数:13
相关论文
共 50 条
  • [1] Neural network-based fault diagnosis for spacecraft with single-gimbal control moment gyros
    Yuandong LI
    Qinglei HU
    Xiaodong SHAO
    [J]. Chinese Journal of Aeronautics., 2022, 35 (07) - 273
  • [2] Neural network-based fault diagnosis for spacecraft with single-gimbal control moment gyros
    LI, Yuandong
    Hu, Qinglei
    Shao, Xiaodong
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2022, 35 (07) : 261 - 273
  • [3] Disturbance Observer-Based Attitude Control of Spacecraft with Single-Gimbal Control Moment Gyros
    Yan, Ruidong
    Zhong, Wu
    [J]. 2014 11TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA), 2014, : 3107 - 3111
  • [4] Rate Damping of a Spacecraft Using Two Single-Gimbal Control Moment Gyros
    Yamada, Katsuhiko
    Jikuya, Ichiro
    Kwak, Okgyu
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2013, 36 (06) : 1606 - 1623
  • [5] Spacecraft attitude maneuver using two single-gimbal control moment gyros
    Kasai, Shinya
    Kojima, Hirohisa
    Satoh, Mitsunori
    [J]. ACTA ASTRONAUTICA, 2013, 84 : 88 - 98
  • [6] Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros
    Gui Haichao
    Jin Lei
    Xu Shijie
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2013, 26 (05) : 1218 - 1226
  • [7] Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros
    Gui Haichao
    Jin Lei
    Xu Shijie
    [J]. Chinese Journal of Aeronautics, 2013, (05) : 1218 - 1226
  • [8] Local controllability and stabilization of spacecraft attitude by two single-gimbal control moment gyros
    Gui Haichao
    Jin Lei
    Xu Shijie
    [J]. Chinese Journal of Aeronautics., 2013, 26 (05) - 1226
  • [9] Two Parallel Single-Gimbal Control Moment Gyros Actuated Spacecraft Attitude Maneuver
    Yue, Chengfei
    Wu, Fan
    Wang, Feng
    Cao, Xibin
    Shen, Qiang
    Kumar, Krishna Dev
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2020, 56 (05) : 4112 - 4123
  • [10] Survey of theory and steering laws of single-gimbal control moment gyros
    Kurokawa, Haruhisa
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (05) : 1331 - 1340