Sliding-mode controller design for spacecraft attitude tracking maneuvers

Yon-Ping Chen*, Shih Cho Lo

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Scopus citations

Abstract

This paper presents a robust sliding-mode control law to deal with the spacecraft attitude tracking problems. Two important natural properties related to the spacecraft model of motion are shown and then by using these properties and the second method of Lyapunov theory, the system stability in the sliding mode can be easily achieved.

Original languageEnglish
Title of host publicationAmerican Control Conference
Editors Anon
PublisherPubl by IEEE
Pages195-196
Number of pages2
ISBN (Print)0780308611
DOIs
StatePublished - 1 Dec 1993
EventProceedings of the 1993 American Control Conference Part 3 (of 3) - San Francisco, CA, USA
Duration: 2 Jun 19934 Jun 1993

Publication series

NameAmerican Control Conference

Conference

ConferenceProceedings of the 1993 American Control Conference Part 3 (of 3)
CitySan Francisco, CA, USA
Period2/06/934/06/93

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