Fault-tolerant control of satellite attitude control systems: Review

被引：0
|
作者：
Jiang B. [1 ]
Zhang K. [1 ]
Yang H. [1 ]
Cheng Y. [1 ]
Ma Y. [1 ]
Cheng W. [1 ]
机构：
[1] College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 11期
基金：
中国国家自然科学基金;
关键词：
Fault-tolerant control; Reconfigurability; Satellite attitude control systems; Satellite formation; Transient and steady-state performances;
D O I：
10.7527/S1000-6893.2020.24662
中图分类号：
学科分类号：
摘要：
The achievements in the research field of fault-tolerant control of satellite attitude systems are reviewed. The results of satellite attitude fault-tolerant control at home and abroad are summarized and analyzed from three parts: the reconfigurability of satellite attitude systems, single satellite fault-tolerant control, and satellite formation fault-tolerant control. The reconfigurability of the satellite attitude system is analyzed from two aspects: reconstruction goals and system functional requirements. The introduction of the current status of single satellite fault-tolerant control mainly includes the adaptive technology, sliding mode theory, prescribed performance, disturbance observer and fault estimation observer. The satellite formation fault-tolerant control methods are explained from the perspectives of independent fault tolerance, cooperative fault tolerance, topology reconstruction, and composition reconstruction. Finally, a summary of this article is provided, and new problems and research ideas in fault-tolerant control of satellite attitude control systems are prospected. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
引用
收藏
相关论文
共 74 条
  • [31] MA Y J, JIANG B, TAO G, Et al., Adaptive direct compensation control scheme for spacecraft with multiple actuator faults, Journal of Guidance, Control, and Dynamics, 42, 4, pp. 923-930, (2019)
  • [32] SUN L., Adaptive fault-tolerant constrained control of cooperative spacecraft rendezvous and docking, IEEE Transactions on Industrial Electronics, 67, 4, pp. 3107-3115, (2020)
  • [33] ZHOU N, KAWANO Y, CAO M., Neural network-based adaptive control for spacecraft under actuator failures and input saturations, IEEE Transactions on Neural Networks and Learning Systems, 31, 9, pp. 3696-3710, (2020)
  • [34] MA Y J, JIANG B, TAO G, Et al., Uncertainty decomposition-based fault-tolerant adaptive control of flexible spacecraft, IEEE Transactions on Aerospace and Electronic Systems, 51, 2, pp. 1053-1068, (2015)
  • [35] ZHAO D, YANG H, JIANG B, Et al., Attitude stabilization of a flexible spacecraft under actuator complete failure, Acta Astronautica, 123, pp. 129-136, (2016)
  • [36] LI Q, YANG H, ZHAO D, Et al., Fault-tolerant control and vibration suppression of flexible spacecraft: an interconnected system approach, Chinese Journal of Aeronautics, 33, 7, pp. 2014-2023, (2020)
  • [37] QIAN M S, SHI Y, GAO Z F, Et al., Integrated fault tolerant tracking control for rigid spacecraft using fractional order sliding mode technique, Journal of the Franklin Institute, 357, 15, pp. 10557-10583, (2020)
  • [38] GAO C Y, DUAN G R., Fault diagnosis and fault tolerant control for nonlinear satellite attitude control systems, Aerospace Science and Technology, 33, 1, pp. 9-15, (2014)
  • [39] SHEN Q, WANG D W, ZHU S Q, Et al., Finite-time fault-tolerant attitude stabilization for spacecraft with actuator saturation, IEEE Transactions on Aerospace and Electronic Systems, 51, 3, pp. 2390-2405, (2015)
  • [40] WANG H, HU Q L, SHI Z, Et al., Backstepping-based finite-time fault-tolerant attitude tracking control for spacecraft, Acta Aeronautica et Astronautica Sinica, 36, 6, pp. 1933-1939, (2015)
12345678