Fault Tolerant Control with TSM for Spacecraft Formation Flying

摘要：

　　In this paper,a fault tolerant-based adaptive terminal sliding mode(TSM)control method is proposed for leader–follower spacecraft formation flying system in the presence of actuator fault.Unknown external disturbances and minimum fault information are adapted online and the great robustness is guaranteed.It has been proved that with this designed controller,the practical finite-time stability(PFS)of the closed-loop system can be guaranteed.Simulation results show the effectiveness of the proposed method.

关键词： Fault tolerant control Spacecraft formation Terminal sliding mode Adaptive control

作者: Xiaoyu Han Yingmin Jia

作者单位: The Seventh Research Division and the Department of Systems and Control,Beijing University of Aeronautics and Astronautics,Xinzhu Building,NO 37 Xueyuan Road,Beijing F907,Haidian District,China

会议类型: 国际会议

会议名称: The 2015 Chinese Intelligent Automation Conference(2015中国智能自动化会议)

会议地点: 福州

会议语种:英文

页码: 243-254

在线出版日期: 2015-05-08（万方平台首次上网日期，不代表论文的发表时间）