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.
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