The stability evolution of a family of simply periodic lunar orbits

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorWinter, Othon C.
dc.date2014-05-27T11:19:51Z
dc.date2016-10-25T18:16:10Z
dc.date2014-05-27T11:19:51Z
dc.date2016-10-25T18:16:10Z
dc.date2000-01-01
dc.date.accessioned2017-04-06T00:56:07Z
dc.date.available2017-04-06T00:56:07Z
dc.identifierPlanetary and Space Science, v. 48, n. 1, p. 23-28, 2000.
dc.identifier0032-0633
dc.identifierhttp://hdl.handle.net/11449/66042
dc.identifierhttp://acervodigital.unesp.br/handle/11449/66042
dc.identifier10.1016/S0032-0633(99)00082-3
dc.identifierWOS:000085251700003
dc.identifier2-s2.0-0010692118
dc.identifierhttp://dx.doi.org/10.1016/S0032-0633(99)00082-3
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/887679
dc.descriptionThe present work deals with a family of simply periodic orbits around the Moon in the rotating Earth Moon-particle system. Taking the framework of the planar, circular, restricted three-body problem, we follow the evolution of this family of periodic orbits using the numerical technique of Poincaré surface of section. The maximum amplitude of oscillation about the periodic orbits are determined and can be used as a parameter to measure the degree of stability in the phase space for such orbits. Despite the fact that the whole family of periodic orbits remain stable, there is a dichotomy in the quasi-periodic ones at the Jacobi constant Cj = 2.85. The quasi-periodic orbits with Cj < 2.85 oscillate around the periodic orbits in a different way from those with Cj > 2.85. © 1999 Elsevier Science Ltd. All rights reserved.
dc.languageeng
dc.relationPlanetary and Space Science
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectPeriodic orbits
dc.subjectStability
dc.subjectSurface of section
dc.titleThe stability evolution of a family of simply periodic lunar orbits
dc.typeOtro


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