Robust Sliding Mode Tracking Control for Linear Tethered Satellite Formation Deployment

Wang Ben, Wang Changqing, Li Aijun, Yu M. Zabolotnov

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, the deployment process of linear tethered satellite formation system is studied. The scheme of phased deployment of formation system is introduced. The nominal model of the formation system is established by Lagrange’s equation, and the nominal trajectory of the tethered satellite formation system is obtained by parameter optimization based on the nominal model. Considering the influence of tether elasticity, possible slack and deformation of tether and dynamics of tether deployment control mechanism, the actual model of the formation system is built by Newton’s second law in the inertial system. Based on the actual model of the system, a robust sliding mode tracking controller is designed to track the optimal nominal trajectory. The simulation results show that the designed controller can accurately track the optimal nominal trajectory in the presence of external disturbances and has strong anti-interference ability and robustness during the deployment process of tethered satellite formation system.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020
编辑Liang Yan, Haibin Duan, Xiang Yu
出版商Springer Science and Business Media Deutschland GmbH
3435-3447
页数13
ISBN(印刷版)9789811581540
DOI
出版状态已出版 - 2022
活动International Conference on Guidance, Navigation and Control, ICGNC 2020 - Tianjin, 中国
期限: 23 10月 202025 10月 2020

出版系列

姓名Lecture Notes in Electrical Engineering
644 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 2020
国家/地区中国
Tianjin
时期23/10/2025/10/20

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