Robust attitude control for spacecraft

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

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-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 languageEnglish
Title of host publicationProceedings of the American Control Conference
Pages1342-1347
Number of pages6
Volume2
DOIs
StatePublished - 1 Jan 2002

Fingerprint Dive into the research topics of 'Robust attitude control for spacecraft'. Together they form a unique fingerprint.

Cite this