Third-body perturbation in the case of elliptic orbits for the disturbing body

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dc.contributor.authorDe Cássia Domingos, Rita [UNESP]
dc.contributor.authorDe Moraes, Rodolpho Vilhena [UNESP]
dc.contributor.authorDe Almeida Prado, Antonio Fernando Bertachini [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionInstituto Nacional de Pesquisas Espaciais (INPE)
dc.date.accessioned2014-05-27T11:23:49Z
dc.date.available2014-05-27T11:23:49Z
dc.date.issued2008-12-01
dc.description.abstractIn the present work it is presented a semi-analytical and a numerical study of the perturbation caused in a spacecraft by a third body using a double averaged analytical model with the disturbing function expanded in Legendre polynomials up to the second-order. The important reason for this procedure is to eliminate the terms due to the short time periodic motion of the spacecraft and to show smooth curves for the evolution of the mean orbital elements for a long time period. The aim of this study is to calculate the effect of lunar perturbations on the orbits of spacecrafts that are traveling around the Earth. It is presented an analysis of the stability of a near-circular orbit and a study to know under which conditions this orbit remains near-circular. A study of the equatorial orbits is also performed.en
dc.description.affiliationGrupo de Dinâmica Orbital e Planetologia UNESP, Guaratinguetá SP
dc.description.affiliationInstituto Nacional de Pesquisas Espaciais, São José dos Campos - SP
dc.description.affiliationUnespGrupo de Dinâmica Orbital e Planetologia UNESP, Guaratinguetá SP
dc.format.extent2639-2652
dc.identifierhttp://www.univelt.com/book=1919
dc.identifier.citationAdvances in the Astronautical Sciences, v. 129 PART 3, p. 2639-2652.
dc.identifier.issn0065-3438
dc.identifier.lattes7740917144757410
dc.identifier.orcid0000-0003-1289-8332
dc.identifier.scopus2-s2.0-60349102909
dc.identifier.urihttp://hdl.handle.net/11449/70861
dc.identifier.wosWOS:000257272902039
dc.language.isoeng
dc.relation.ispartofAdvances in the Astronautical Sciences
dc.relation.ispartofsjr0,187
dc.rights.accessRightsAcesso aberto
dc.sourceScopus
dc.subjectAnalytical models
dc.subjectDisturbing functions
dc.subjectElliptic orbits
dc.subjectEquatorial orbits
dc.subjectLegendre polynomials
dc.subjectNear-circular orbits
dc.subjectNumerical studies
dc.subjectOrbital elements
dc.subjectPeriodic motions
dc.subjectSecond orders
dc.subjectSemi-analytical
dc.subjectSmooth curves
dc.subjectThird bodies
dc.subjectThird-body perturbations
dc.subjectTime periods
dc.subjectAstrophysics
dc.subjectDynamics
dc.subjectSpacecraft
dc.subjectOrbits
dc.titleThird-body perturbation in the case of elliptic orbits for the disturbing bodyen
dc.typeTrabalho apresentado em evento
unesp.author.lattes7740917144757410[2]
unesp.author.orcid0000-0003-1289-8332[2]
unesp.campusUniversidade Estadual Paulista (Unesp), Faculdade de Engenharia, Guaratinguetápt

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