Alternative paths for insertion of probes into high inclination lunar orbits

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dc.contributor.authorde Melo, C. F.
dc.contributor.authorMacau, E. E. N.
dc.contributor.authorWinter, O. C. [UNESP]
dc.contributor.authorNeto, E. Vielra [UNESP]
dc.contributor.institutionInstituto Nacional de Pesquisas Espaciais (INPE)
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-05-20T15:19:26Z
dc.date.available2014-05-20T15:19:26Z
dc.date.issued2007-01-01
dc.description.abstractThe dynamics of the restricted three-body Earth-Moon-particle problem predicts the existence of direct periodic orbits around the Lagrangian equilibrium point L1. From these orbits, we derive a set of trajectories that form links between the Earth and the Moon and are capable of performing transfers between terrestrial and lunar orbits, in addition to defining an escape route from the Earth-Moon system. When we consider a more complex and realistic dynamical system - the four-body Sun-Earth-Moon-particle (probe) problem - the trajectories have an expressive gain of inclination when they penetrate in the lunar influence sphere, thus allowing the insertion of probes into low-altitude lunar orbits with high inclinations, including polar orbits. In this study, we present these links and investigate some possibilities for performing an Earth-Moon transfer based on these trajectories. (C) 2007 COSPAR. Published by Elsevier Ltd. All rights reserved.en
dc.description.affiliationInst Nacl Pesquisas Espaciais, BR-12227010 Sao Jose Dos Campos, Brazil
dc.description.affiliationUNESP, Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP, Brazil
dc.description.affiliationUnespUNESP, Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP, Brazil
dc.format.extent58-68
dc.identifierhttp://dx.doi.org/10.1016/j.asr.2007.03.020
dc.identifier.citationAdvances In Space Research. Oxford: Elsevier B.V., v. 40, n. 1, p. 58-68, 2007.
dc.identifier.doi10.1016/j.asr.2007.03.020
dc.identifier.issn0273-1177
dc.identifier.lattes0960024575647258
dc.identifier.urihttp://hdl.handle.net/11449/30911
dc.identifier.wosWOS:000253589100008
dc.language.isoeng
dc.publisherElsevier B.V.
dc.relation.ispartofAdvances in Space Research
dc.relation.ispartofjcr1.529
dc.relation.ispartofsjr0,569
dc.rights.accessRightsAcesso restrito
dc.sourceWeb of Science
dc.subjectastrodynamicspt
dc.subjectmission designpt
dc.subjectearth-moon transferpt
dc.subjectorbital maneuverspt
dc.titleAlternative paths for insertion of probes into high inclination lunar orbitsen
dc.typeArtigo
dcterms.licensehttp://www.elsevier.com/about/open-access/open-access-policies/article-posting-policy
dcterms.rightsHolderElsevier B.V.
unesp.author.lattes0960024575647258
unesp.campusUniversidade Estadual Paulista (Unesp), Faculdade de Engenharia, Guaratinguetápt

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