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dc.contributor.authorMoraes, R. Vilhena de
dc.contributor.authorSilva, P. A. F. da [UNESP]
dc.date.accessioned2014-05-27T06:09:36Z
dc.date.available2014-05-27T06:09:36Z
dc.date.issued1989-09-01
dc.identifierhttp://dx.doi.org/10.1007/BF00053453
dc.identifier.citationCelestial Mechanics and Dynamical Astronomy, v. 47, n. 3, p. 225-243, 1989.
dc.identifier.issn0923-2958
dc.identifier.issn1572-9478
dc.identifier.urihttp://hdl.handle.net/11449/63909
dc.description.abstractUsing Hamiltonian formalism the translational-rotational motion of a satellite is studied near a resonance considering the orbital and rotational motions. A first order perturbation theory is derived by Hori's transformation in order to eliminate short and long periodic terms, preserving in the new Hamiltonian secular and resonant terms. This theory is again applied to study the resonant system whose analysis lead us to a system of equations equivalent to the equations of a simple pendulum which is integrable in terms of elliptical integrals. © 1990 Kluwer Academic Publishers.en
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.format.extent225-243
dc.language.isoeng
dc.relation.ispartofCelestial Mechanics and Dynamical Astronomy
dc.sourceScopus
dc.titleInfluence of the resonance in a gravity-gradient stabilized satelliteen
dc.typeArtigo
dcterms.licensehttp://www.springer.com/open+access/authors+rights
dc.contributor.institutionInstituto Tecnológico de Aeronáutica
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.description.affiliationDepartamento de Mecânica de Vôo e Orbital Instituto Tecnológico de Aeronáutica, 12225-São Jose dos Campos-SP
dc.description.affiliationInstituto de Geociências e Ciências Exatas UNESP, Rio Claro-SP
dc.description.affiliationUnespInstituto de Geociências e Ciências Exatas UNESP, Rio Claro-SP
dc.identifier.doi10.1007/BF00053453
dc.identifier.wosWOS:000207114300001
dc.rights.accessRightsAcesso restrito
dc.description.sponsorshipIdFAPESP: 85/2699-0
dc.identifier.scopus2-s2.0-34249958718
dc.relation.ispartofjcr2.121
dc.relation.ispartofsjr1,092
dc.relation.ispartofsjr1,092
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