Full metadata record
DC FieldValueLanguage
dc.contributor.authorGe, ZMen_US
dc.contributor.authorChen, HKen_US
dc.date.accessioned2014-12-08T15:02:59Z-
dc.date.available2014-12-08T15:02:59Z-
dc.date.issued1996en_US
dc.identifier.issn0954-4100en_US
dc.identifier.urihttp://hdl.handle.net/11536/1580-
dc.identifier.urihttp://dx.doi.org/10.1243/PIME_PROC_1996_210_344_02en_US
dc.description.abstractSufficient conditions for the global stabilities of equilibrium positions of a dual-spin satellite equipped with a cylindrical electrostatic screen normal to the circular equatorial orbital plane system under the action of moments induced by the gravitational and Lorentz forces are obtained by Liapunov's direct method. The problem is then studied with respect to all variables, including the angular velocity of the rotor. The instabilities of the problem are solved by the first approximation theorem. Furthermore, sufficient conditions for the global stability of rotation with arbitrary angular velocity for an axisymmetric dual-spin satellite equipped with an electrostatic screen me presented by applying Liapunov's direct method.en_US
dc.language.isoen_USen_US
dc.subjectshielded dual-spin satelliteen_US
dc.subjectLiapunov's direct methoden_US
dc.subjectglobal stabilityen_US
dc.titleGlobal stability of a shielded dual-spin satelliteen_US
dc.typeArticleen_US
dc.identifier.doi10.1243/PIME_PROC_1996_210_344_02en_US
dc.identifier.journalPROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERINGen_US
dc.citation.volume210en_US
dc.citation.issueG1en_US
dc.citation.spage53en_US
dc.citation.epage63en_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:A1996TX72500007-
dc.citation.woscount0-
Appears in Collections:Articles