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Event-Triggered Finite-Time Adaptive Coordinated Control for Spacecraft Formation Flying Under Actuator Faults

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

For attitude coordination tracking of spacecraft formation flying affected by external disturbances, actuator faults, and limited communication, this paper investigates a finite-time adaptive coordinated control law. To suppress the influence of external disturbances and actuator faults, an adaptive sliding mode controller is adopted. To reduce the communication between neighboring spacecraft, a distributed event-triggered control scheme is designed. Under the scheme, the communication channel only transmits information at the trigger instants that are decided by the predefined triggering condition. Based on the Lyapunov theorem, the stability of the closed-loop system can be proved. The effectiveness of the scheme is verified by simulation results.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
编辑Liang Yan, Haibin Duan, Yimin Deng, Liang Yan
出版商Springer Science and Business Media Deutschland GmbH
2043-2052
页数10
ISBN(印刷版)9789811966125
DOI
出版状态已出版 - 2023
活动International Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, 中国
期限: 5 8月 20227 8月 2022

出版系列

姓名Lecture Notes in Electrical Engineering
845 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2022
国家/地区中国
Harbin
时期5/08/227/08/22

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