DUGiDocsJ2 effect and elliptic inclined periodic orbits in the collision three-body problem
dc.contributor.author
dc.date.accessioned
2014-03-24T11:50:45Z
dc.date.available
2014-03-24T11:50:45Z
dc.date.issued
2008
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1536-0040
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dc.description.abstract
The existence of a new class of inclined periodic orbits of the collision restricted three-body problem is shown. The symmetric periodic solutions found are perturbations of elliptic kepler orbits and they exist only for special values of the inclination and are related to the motion of a satellite around an oblate planet
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application/pdf
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eng
dc.publisher
Society for Industrial and Applied Mathematics (SIAM)
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Reproducció digital del document publicat a: http://dx.doi.org/10.1137/070683854
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© SIAM journal on applied dynamical systems, 2008, vol. 7, núm. 1, p. 1-17
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Articles publicats (D-IMA)
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Tots els drets reservats
dc.title
J2 effect and elliptic inclined periodic orbits in the collision three-body problem
dc.type
info:eu-repo/semantics/article
dc.rights.accessRights
info:eu-repo/semantics/openAccess
dc.embargo.terms
Cap
dc.type.version
info:eu-repo/semantics/acceptedVersion
dc.identifier.doi
dc.identifier.idgrec
007997