Improved stability of a dual-spin satellite in circular orbit

完整後設資料紀錄

DC 欄位	值	語言
dc.contributor.author	Ge, ZM	en_US
dc.contributor.author	Chen, HK	en_US
dc.date.accessioned	2014-12-08T15:02:03Z	-
dc.date.available	2014-12-08T15:02:03Z	-
dc.date.issued	1997-02-01	en_US
dc.identifier.issn	0021-4922	en_US
dc.identifier.uri	http://hdl.handle.net/11536/764	-
dc.description.abstract	Sufficient conditions for the global stability of equilibrium positions of a dual-spin satellite in a circular orbital system in a Newtonian central force field are obtained by Liapunov's direct method. The new results are compared with those already known. The problem is then studied with respect to all variables, including the angular velocity of the rotor. Further, sufficient conditions for the global stability of rotation with arbitrary angular velocity for an axisymmetric dual-spin satellite are presented by Liapunov's direct method, which improve on Kane's result of infinitesimal stability obtained by linearized equations of motion.	en_US
dc.language.iso	en_US	en_US
dc.subject	global stability	en_US
dc.subject	dual-spin satellite	en_US
dc.subject	Liapunov's direct method	en_US
dc.title	Improved stability of a dual-spin satellite in circular orbit	en_US
dc.type	Article	en_US
dc.identifier.journal	JAPANESE JOURNAL OF APPLIED PHYSICS PART 1-REGULAR PAPERS SHORT NOTES & REVIEW PAPERS	en_US
dc.citation.volume	36	en_US
dc.citation.issue	2	en_US
dc.citation.spage	948	en_US
dc.citation.epage	956	en_US
dc.contributor.department	交大名義發表	zh_TW
dc.contributor.department	機械工程學系	zh_TW
dc.contributor.department	National Chiao Tung University	en_US
dc.contributor.department	Department of Mechanical Engineering	en_US
dc.identifier.wosnumber	WOS:A1997WN16000066	-
dc.citation.woscount	0	-
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