dc.contributorUNESP Univ Estadual Paulista
dc.contributorITA Inst Tecnol Aeronaut
dc.contributorUniversidade Federal de São Paulo (UNIFESP)
dc.creatorSampaio, J. C.
dc.creatorNeto, A. G. S.
dc.creatorFernandes, S. S.
dc.creatorVilhena de Moraes, R. [UNIFESP]
dc.creatorTerra, M. O.
dc.date.accessioned2016-01-24T14:28:05Z
dc.date.accessioned2022-10-07T20:46:52Z
dc.date.available2016-01-24T14:28:05Z
dc.date.available2022-10-07T20:46:52Z
dc.date.created2016-01-24T14:28:05Z
dc.date.issued2012-12-01
dc.identifierActa Astronautica. Oxford: Pergamon-Elsevier B.V., v. 81, n. 2, p. 623-634, 2012.
dc.identifier0094-5765
dc.identifierhttp://repositorio.unifesp.br/handle/11600/35553
dc.identifier10.1016/j.actaastro.2012.08.025
dc.identifierWOS:000311467200024
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/4022755
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 B.V. All rights reserved.
dc.languageeng
dc.publisherElsevier B.V.
dc.relationActa Astronautica
dc.rightshttp://www.elsevier.com/about/open-access/open-access-policies/article-posting-policy
dc.rightsAcesso restrito
dc.subjectArtificial satellites
dc.subjectResonance
dc.subjectOrbits
dc.titleArtificial satellites orbits in 2:1 resonance: GPS constellation
dc.typeArtigo


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