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

Department of Electrical and Computer Engineering

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

9 Scopus citations

Abstract

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.

Original language	English
Title of host publication	Proceedings of the American Control Conference
Pages	1342-1347
Number of pages	6
Volume	2
DOIs	https://doi.org/10.1109/ACC.2002.1023207
State	Published - 8 May 2002

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10.1109/ACC.2002.1023207

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title = "Robust attitude control for spacecraft",

abstract = "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.",

author = "Yew-Wen Liang and Chu, {Tzu Chiang} and Cheng, {Chiz Chung}",

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N2 - 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.

AB - 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.

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Robust attitude control for spacecraft

Abstract

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