Stability of an elastically connected two-body space station by the perturbation method

doi:10.1243/0954410971532613

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DC 欄位	值	語言
dc.contributor.author	Ge, ZM	en_US
dc.contributor.author	Ku, SC	en_US
dc.date.accessioned	2014-12-08T15:02:09Z	-
dc.date.available	2014-12-08T15:02:09Z	-
dc.date.issued	1997	en_US
dc.identifier.issn	0954-4100	en_US
dc.identifier.uri	http://hdl.handle.net/11536/847	-
dc.identifier.uri	http://dx.doi.org/10.1243/0954410971532613	en_US
dc.description.abstract	This investigation deals with the stability, in a circular orbit, of a flexible space station consisting of two inertially identical rigid end bodies connected together by an elastic structure. The earth-pointing motion and the rotation with arbitrary initial angular velocity perpendicular to the orbital plane are studied by using the multiple-scales technique. The first-order approximate analytical solution and the conditions of stability are obtained.	en_US
dc.language.iso	en_US	en_US
dc.subject	stability	en_US
dc.subject	space station	en_US
dc.subject	perturbation method	en_US
dc.subject	multiple-scales technique	en_US
dc.title	Stability of an elastically connected two-body space station by the perturbation method	en_US
dc.type	Article	en_US
dc.identifier.doi	10.1243/0954410971532613	en_US
dc.identifier.journal	PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING	en_US
dc.citation.volume	211	en_US
dc.citation.issue	G3	en_US
dc.citation.spage	193	en_US
dc.citation.epage	208	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:A1997XY04500005	-
dc.citation.woscount	0	-
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