Prescribed Perfomance Finite-Time Attitude Tracking Control of Spinning Tether System base on Backstepping Method

Yi Chen, Changqing Wang, Aijun Li, Hao Chang Tian, Ying Zhang

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper mainly focuses on the attitude control of end-body spacecraft during the rotation of spinning tether system (STS). First, the Newton-Euler method is used to establish the kinematics and attitude dynamics models of the spinning tether system. Based on the quaternion theory, the attitude kinematics equations of the tether system described by quaternion are derived, and the closed-loop attitude tracking error model is derived accordingly. Then, a new finite-time performance function (FTPF) is used to design a prescribed performance finite-time attitude controller based on back-stepping method. This controller can make the attitude tracking error converge to the expected region in finite time. Finally, the effectiveness of the proposed method is verified by numerical simulation.

源语言英语
主期刊名Proceeding - 2021 China Automation Congress, CAC 2021
出版商Institute of Electrical and Electronics Engineers Inc.
6850-6855
页数6
ISBN(电子版)9781665426473
DOI
出版状态已出版 - 2021
活动2021 China Automation Congress, CAC 2021 - Beijing, 中国
期限: 22 10月 202124 10月 2021

出版系列

姓名Proceeding - 2021 China Automation Congress, CAC 2021

会议

会议2021 China Automation Congress, CAC 2021
国家/地区中国
Beijing
时期22/10/2124/10/21

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