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dc.contributor.authorRosales, José J.
dc.contributor.authorJorba, Ángel
dc.contributor.authorJorba-Cuscó, Marc
dc.date2021
dc.date.accessioned2022-06-03T10:43:56Z
dc.date.available2022-06-03T10:43:56Z
dc.identifier.issn0923-2958
dc.identifier.urihttps://reunir.unir.net/handle/123456789/13229
dc.description.abstractThis paper deals with direct transfers from the Earth to Halo orbits related to the translunar point. The gravitational influence of the Sun as a fourth body is taken under consideration by means of the Bicircular Problem (BCP), which is a periodic time dependent perturbation of the Restricted Three Body Problem (RTBP) that includes the direct effect of the Sun on the spacecraft. In this model, the Halo family is quasi-periodic. Here we show how the effect of the Sun bends the stable manifolds of the quasi-periodic Halo orbits in a way that allows for direct transfers.es_ES
dc.language.isoenges_ES
dc.publisherSpringer Science and Business Media B.V.es_ES
dc.relation.ispartofseries;vol. 133, nº 11-12
dc.relation.urihttps://link.springer.com/article/10.1007/s10569-021-10054-4es_ES
dc.rightsopenAccesses_ES
dc.subjectbicircular problemes_ES
dc.subjectearth–moon transferses_ES
dc.subjectinvariant manifolds of tories_ES
dc.subjectquasi-periodic halo orbitses_ES
dc.subjecttranslunar pointes_ES
dc.subjectScopuses_ES
dc.subjectJCRes_ES
dc.titleTransfers from the Earth to L2 Halo orbits in the Earth–Moon bicircular problemes_ES
dc.typearticlees_ES
reunir.tag~ARIes_ES
dc.identifier.doihttps://doi.org/10.1007/s10569-021-10054-4


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