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

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorDe Cássia Domingos, Rita
dc.creatorDe Moraes, Rodolpho Vilhena
dc.creatorDe Almeida Prado, Antonio Fernando Bertachini
dc.date2014-05-27T11:23:49Z
dc.date2016-10-25T18:26:41Z
dc.date2014-05-27T11:23:49Z
dc.date2016-10-25T18:26:41Z
dc.date2008-12-01
dc.date.accessioned2017-04-06T01:34:56Z
dc.date.available2017-04-06T01:34:56Z
dc.identifierAdvances in the Astronautical Sciences, v. 129 PART 3, p. 2639-2652.
dc.identifier0065-3438
dc.identifierhttp://hdl.handle.net/11449/70861
dc.identifierhttp://acervodigital.unesp.br/handle/11449/70861
dc.identifierWOS:000257272902039
dc.identifier2-s2.0-60349102909
dc.identifierhttp://www.univelt.com/book=1919
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/891928
dc.descriptionIn 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.
dc.languageeng
dc.relationAdvances in the Astronautical Sciences
dc.rightsinfo:eu-repo/semantics/closedAccess
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 body
dc.typeOtro


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