Zero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon system

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dc.contributor.authorSalazar, F. J. T. [UNESP]
dc.contributor.authorMasdemont, J. J.
dc.contributor.authorGomez, G.
dc.contributor.authorMacau, E. E.
dc.contributor.authorWinter, O. C. [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionETSEIB UPC
dc.contributor.institutionUB
dc.contributor.institutionInst Nacl Pesquisas Espaciais
dc.date.accessioned2015-03-18T15:53:19Z
dc.date.available2015-03-18T15:53:19Z
dc.date.issued2014-11-01
dc.description.abstractAssume a constellation of satellites is flying near a given nominal trajectory around L-4 or L-5 in the Earth-Moon system in such a way that there is some freedom in the selection of the geometry of the constellation. We are interested in avoiding large variations of the mutual distances between spacecraft. In this case, the existence of regions of zero and minimum relative radial acceleration with respect to the nominal trajectory will prevent from the expansion or contraction of the constellation. In the other case, the existence of regions of maximum relative radial acceleration with respect to the nominal trajectory will produce a larger expansion and contraction of the constellation. The goal of this paper is to study these regions in the scenario of the Circular Restricted Three Body Problem by means of a linearization of the equations of motion relative to the periodic orbits around L-4 or L-5. This study corresponds to a preliminar planar formation flight dynamics about triangular libration points in the Earth-Moon system. Additionally, the cost estimate to maintain the constellation in the regions of zero and minimum relative radial acceleration or keeping a rigid configuration is computed with the use of the residual acceleration concept. At the end, the results are compared with the dynamical behavior of the deviation of the constellation from a periodic orbit. (C) 2014 COSPAR. Published by Elsevier Ltd. All rights reserved.en
dc.description.affiliationUNESP, Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP, Brazil
dc.description.affiliationETSEIB UPC, Dept Matemat Aplicada 1, Barcelona 08028, Spain
dc.description.affiliationUB, Dept Matemat Aplicada & Anal, Barcelona 08007, Spain
dc.description.affiliationInst Nacl Pesquisas Espaciais, BR-12227010 Sao Jose Dos Campos, SP, Brazil
dc.description.affiliationUnespUNESP, Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP, Brazil
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.description.sponsorshipConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)
dc.description.sponsorshipMINECO-FEDER
dc.description.sponsorshipCatalan grant
dc.description.sponsorshipIdFAPESP: 08/06066-5
dc.description.sponsorshipIdFAPESP: 11/08171-3
dc.description.sponsorshipIdFAPESP: 11/50151-0
dc.description.sponsorshipIdFAPESP: 13/03233-6
dc.description.sponsorshipIdMINECO-FEDERMTM 2012-31714
dc.description.sponsorshipIdCatalan grant2009SGR-D-D589-E
dc.format.extent1838-1857
dc.identifierhttp://dx.doi.org/10.1016/j.asr.2014.07.018
dc.identifier.citationAdvances In Space Research. Oxford: Elsevier Sci Ltd, v. 54, n. 9, p. 1838-1857, 2014.
dc.identifier.doi10.1016/j.asr.2014.07.018
dc.identifier.issn0273-1177
dc.identifier.lattes0960024575647258
dc.identifier.urihttp://hdl.handle.net/11449/116440
dc.identifier.wosWOS:000344204200012
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.subjectFormation flight of satellitesen
dc.subjectZero Relative Radial Accelerationen
dc.subjectEarth-Moon systemen
dc.subjectCircular Restricted Three Body Problemen
dc.subjectStable Lagrangian pointsen
dc.subjectResidual accelerationen
dc.titleZero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon systemen
dc.typeArtigo
dcterms.licensehttp://www.elsevier.com/about/open-access/open-access-policies/article-posting-policy
dcterms.rightsHolderElsevier B.V.
unesp.author.lattes0960024575647258
unesp.author.orcid0000-0002-4901-3289[5]
unesp.campusUniversidade Estadual Paulista (Unesp), Faculdade de Engenharia, Guaratinguetápt

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