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Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/9280
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dc.contributor.authorSampaio, J. C.-
dc.contributor.authorNeto, A. G. S.-
dc.contributor.authorFernandes, S. S.-
dc.contributor.authorVilhena de Moraes, R.-
dc.contributor.authorTerra, M. O.-
dc.date.accessioned2014-05-20T13:27:58Z-
dc.date.accessioned2016-10-25T16:47:49Z-
dc.date.available2014-05-20T13:27:58Z-
dc.date.available2016-10-25T16:47:49Z-
dc.date.issued2012-12-01-
dc.identifierhttp://dx.doi.org/10.1016/j.actaastro.2012.08.025-
dc.identifier.citationActa Astronautica. Oxford: Pergamon-Elsevier B.V. Ltd, v. 81, n. 2, p. 623-634, 2012.-
dc.identifier.issn0094-5765-
dc.identifier.urihttp://hdl.handle.net/11449/9280-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/9280-
dc.description.abstractIn this work, the resonance problem in the artificial satellites motion is studied. The development of the geopotential includes the zonal harmonics J(20) and J(40) and the tesseral harmonics J(22) and J(42). Through an averaging procedure and successive Mathieu transformations, the order of dynamical system is reduced and the final system is solved by numerical integration. In the simplified dynamical model, three critical angles are studied. The half-width of the separatrix is calculated through a linearized model which describes the behavior of the dynamical system in a neighborhood of each critical angle. Through the resonance overlap criterion the possible regular and irregular motions are investigated by the time behavior of the semi-major axis, argument of perigee and eccentricity. The largest Lyapunov exponent is used as tool to verify the chaotic motion. (C) 2012 Elsevier Ltd. All rights reserved.en
dc.description.sponsorshipFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)-
dc.description.sponsorshipConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)-
dc.format.extent623-634-
dc.language.isoeng-
dc.publisherPergamon-Elsevier B.V. Ltd-
dc.sourceWeb of Science-
dc.subjectArtificial satellitesen
dc.subjectResonanceen
dc.subjectOrbitsen
dc.titleArtificial satellites orbits in 2:1 resonance: GPS constellationen
dc.typeoutro-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.contributor.institutionInstituto Tecnológico de Aeronáutica (ITA)-
dc.contributor.institutionUniversidade Federal de São Paulo (UNIFESP)-
dc.description.affiliationUNESP Univ Estadual Paulista, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.affiliationITA Inst Tecnol Aeronaut, BR-12228900 Sao Jose Dos Campos, SP, Brazil-
dc.description.affiliationUNIFESP Univ Fed São Paulo, BR-12231280 Sao Jose Dos Campos, SP, Brazil-
dc.description.affiliationUnespUNESP Univ Estadual Paulista, BR-12516410 Guaratingueta, SP, Brazil-
dc.description.sponsorshipIdFAPESP: 09/00735-5-
dc.description.sponsorshipIdFAPESP: 06/04997-6-
dc.description.sponsorshipIdCNPq: 300952/2008-2-
dc.description.sponsorshipIdCNPq: 302949/2009-7-
dc.identifier.doi10.1016/j.actaastro.2012.08.025-
dc.identifier.wosWOS:000311467200024-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofActa Astronautica-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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