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dc.contributor.authorLlibre Saló, Jaume
dc.contributor.authorOllé Torner, Mercè
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I
dc.date.accessioned2007-09-28T18:12:31Z
dc.date.available2007-09-28T18:12:31Z
dc.date.issued2001
dc.identifier.urihttp://hdl.handle.net/2117/1193
dc.description.abstractThis paper provides a description of the motion of Saturn coorbital satellites Janus and Epimetheus by means of horseshoe periodic orbits in the framework of the planar restricted three-body problem for the mass parameter . The mechanism of existence of such orbits for any value of and the Jacobi constant C close to C(L3), L3 being an adequate collinear equilibrium point, is analyzed from two different points of view and a systematic way to compute the horseshoe periodic orbits is also described.
dc.format.extent13 pages
dc.language.isoeng
dc.rightsAttribution-NonCommercial-NoDerivs 2.5 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/2.5/es/
dc.subject.lcshDynamics
dc.subject.lcshAstronomy and astrophysics
dc.subject.otherCelestial mechanics
dc.subject.otherPlanets and Satellites
dc.subject.otherSolar system
dc.titleThe motion of Saturn coorbital satellites in the restricted three-body problem
dc.typeArticle
dc.subject.lemacPartícules (Física nuclear)
dc.subject.lemacAstronomia
dc.subject.lemacAstrofísica
dc.contributor.groupUniversitat Politècnica de Catalunya. EGSA - Equacions Diferencials, Geometria, Sistemes Dinàmics i de Control, i Aplicacions
dc.subject.amsClassificació AMS::70 Mechanics of particles and systems::70F Dynamics of a system of particles, including celestial mechanics
dc.subject.amsClassificació AMS::85 Astronomy and astrophysics
dc.rights.accessOpen Access


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Except where otherwise noted, content on this work is licensed under a Creative Commons license: Attribution-NonCommercial-NoDerivs 2.5 Spain