dc.contributorUniversidade Estadual Paulista (Unesp)
dc.date.accessioned2014-02-26T17:29:06Z
dc.date.accessioned2014-05-20T14:15:57Z
dc.date.available2014-02-26T17:29:06Z
dc.date.available2014-05-20T14:15:57Z
dc.date.created2014-02-26T17:29:06Z
dc.date.created2014-05-20T14:15:57Z
dc.date.issued2007-05-01
dc.identifierCelestial Mechanics & Dynamical Astronomy. Dordrecht: Springer, v. 98, n. 1, p. 5-30, 2007.
dc.identifier0923-2958
dc.identifierhttp://hdl.handle.net/11449/24783
dc.identifier10.1007/s10569-007-9066-9
dc.identifierWOS:000245966700002
dc.identifier5483476857978177
dc.description.abstractThe dynamics of a pair of satellites similar to Enceladus-Dione is investigated with a two-degrees-of-freedom model written in the domain of the planar general three-body problem. Using surfaces of section and spectral analysis methods, we study the phase space of the system in terms of several parameters, including the most recent data. A detailed study of the main possible regimes of motion is presented, and in particular we show that, besides the two separated resonances, the phase space is replete of secondary resonances.
dc.languageeng
dc.publisherSpringer
dc.relationCelestial Mechanics & Dynamical Astronomy
dc.relation2.121
dc.relation1,092
dc.rightsAcesso restrito
dc.sourceWeb of Science
dc.subjectEnceladus
dc.subjectDione
dc.subjectMean-Motion resonance
dc.subjectperiodic orbits
dc.subjectregular and chaotic motion
dc.subjectsecondary resonance
dc.subjectSaturn
dc.titleDynamics of two satellites in the 2/1 Mean-Motion resonance: application to the case of Enceladus and Dione
dc.typeArtículos de revistas


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