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dc.contributor.authorGe, ZMen_US
dc.contributor.authorKu, SCen_US
dc.date.accessioned2014-12-08T15:02:09Z-
dc.date.available2014-12-08T15:02:09Z-
dc.date.issued1997en_US
dc.identifier.issn0954-4100en_US
dc.identifier.urihttp://hdl.handle.net/11536/847-
dc.identifier.urihttp://dx.doi.org/10.1243/0954410971532613en_US
dc.description.abstractThis 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.isoen_USen_US
dc.subjectstabilityen_US
dc.subjectspace stationen_US
dc.subjectperturbation methoden_US
dc.subjectmultiple-scales techniqueen_US
dc.titleStability of an elastically connected two-body space station by the perturbation methoden_US
dc.typeArticleen_US
dc.identifier.doi10.1243/0954410971532613en_US
dc.identifier.journalPROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERINGen_US
dc.citation.volume211en_US
dc.citation.issueG3en_US
dc.citation.spage193en_US
dc.citation.epage208en_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.departmentNational Chiao Tung Universityen_US
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:A1997XY04500005-
dc.citation.woscount0-
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