Minimum-time spacecraft maneuver using sliding-mode control

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DC Field	Value	Language
dc.contributor.author	Jan, YW	en_US
dc.contributor.author	Chiou, JC	en_US
dc.date.accessioned	2014-12-08T15:39:46Z	-
dc.date.available	2014-12-08T15:39:46Z	-
dc.date.issued	2004-01-01	en_US
dc.identifier.issn	0094-5765	en_US
dc.identifier.uri	http://dx.doi.org/10.1016/S0094-5765(03)00194-2	en_US
dc.identifier.uri	http://hdl.handle.net/11536/27166	-
dc.description.abstract	The purpose of this paper is to present a sliding mode control method that can be used to perform a spacecraft large angle maneuver with minimum time. An algorithm of minimum-time SMC is developed to provide the robust tracking control. The simulation results are compared with previous developed control schemes, eigenaxis quaternion regulator, to demonstrate the superiority of the proposed sliding mode control algorithm. (C) 2003 Elsevier Ltd. All rights reserved.	en_US
dc.language.iso	en_US	en_US
dc.title	Minimum-time spacecraft maneuver using sliding-mode control	en_US
dc.type	Article	en_US
dc.identifier.doi	10.1016/S0094-5765(03)00194-2	en_US
dc.identifier.journal	ACTA ASTRONAUTICA	en_US
dc.citation.volume	54	en_US
dc.citation.issue	1	en_US
dc.citation.spage	69	en_US
dc.citation.epage	75	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:000186017700006	-
dc.citation.woscount	3	-
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APA	Jan, Y., & Chiou, J. (2004). Minimum-time spacecraft maneuver using sliding-mode control. WOS:000186017700006.
Bibtex	@article{Jan2004Minimum-time, title={Minimum-time spacecraft maneuver using sliding-mode control}, author={Jan, YW and Chiou, JC}, journal={WOS:000186017700006}, year={2004}, url={https://ir.lib.nycu.edu.tw/handle/11536/27166?mode=full}, }