Robust attitude control for spacecraft

完整後設資料紀錄

DC 欄位	值	語言
dc.contributor.author	Liang, YW	en_US
dc.contributor.author	Chu, TC	en_US
dc.contributor.author	Cheng, CC	en_US
dc.date.accessioned	2014-12-08T15:26:28Z	-
dc.date.available	2014-12-08T15:26:28Z	-
dc.date.issued	2002	en_US
dc.identifier.isbn	0-7803-7298-0	en_US
dc.identifier.issn	0743-1619	en_US
dc.identifier.uri	http://hdl.handle.net/11536/18788	-
dc.description.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.	en_US
dc.language.iso	en_US	en_US
dc.title	Robust attitude control for spacecraft	en_US
dc.type	Proceedings Paper	en_US
dc.identifier.journal	PROCEEDINGS OF THE 2002 AMERICAN CONTROL CONFERENCE, VOLS 1-6	en_US
dc.citation.spage	1342	en_US
dc.citation.epage	1347	en_US
dc.contributor.department	電控工程研究所	zh_TW
dc.contributor.department	Institute of Electrical and Control Engineering	en_US
dc.identifier.wosnumber	WOS:000178974700232	-
顯示於類別：	會議論文