Robust attitude control for spacecraft

Yew-Wen Liang; Tzu Chiang Chu; Chiz Chung Cheng

doi:10.1109/ACC.2002.1023207

Robust attitude control for spacecraft

Yew-Wen Liang, Tzu Chiang Chu, Chiz Chung Cheng

電機工程學系

研究成果: Chapter › 同行評審

9 引文斯高帕斯（Scopus）

摘要

This paper deals with the spacecraft attitude tracking problems in the presence of model uncertainties and external disturbances. A modified VSC design scheme is proposed by the use of Variable Structure Control (VSC) design technique. These modified VSC laws are continuous, which are shown able to alleviate chattering drawback inherited from sign-type VSC controllers and enhance the uniformly ultimate boundedness performance suffered by saturation-type ones to asymptotic stability level. Numerical simulations are also given to demonstrate the benefits of the proposed VSC scheme.

原文	English
主出版物標題	Proceedings of the American Control Conference
頁面	1342-1347
頁數	6
卷	2
DOIs	https://doi.org/10.1109/ACC.2002.1023207
出版狀態	Published - 8 5月 2002

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10.1109/ACC.2002.1023207

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Robust attitude control for spacecraft

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