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Passivity-Based Adaptive Internal Model Attitude Tracking Control of Uncertain Rigid Spacecraft

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The problems of a spacecraft attitude tracking and disturbance rejection are considered. Attitude tracking dynamics are formulated with typical Euler-Lagrange form, and a nonlinear controller is designed by combining a passivity-based adaptive method with an internal model. The unknown constant disturbance and inertia uncertainties are estimated online by element-wise adaptive update laws, while the unknown periodic disturbance is compensated by the internal model. Asymptotic stability of the closed-loop system is proved in the Lyapunov framework. A numerical example is also given to validate the theoretical results of this work.

源语言英语
主期刊名Proceedings of the 37th Chinese Control Conference, CCC 2018
编辑Xin Chen, Qianchuan Zhao
出版商IEEE Computer Society
9742-9747
页数6
ISBN(电子版)9789881563941
DOI
出版状态已出版 - 5 10月 2018
活动37th Chinese Control Conference, CCC 2018 - Wuhan, 中国
期限: 25 7月 201827 7月 2018

出版系列

姓名Chinese Control Conference, CCC
2018-July
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议37th Chinese Control Conference, CCC 2018
国家/地区中国
Wuhan
时期25/07/1827/07/18

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