The motion of Saturn coorbital satellites in the restricted three-body problem

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To access the full text documents, please follow this link: http://hdl.handle.net/2117/1193

dc.contributor	Universitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I
dc.contributor	Universitat Politècnica de Catalunya. EGSA - Equacions Diferencials, Geometria, Sistemes Dinàmics i de Control, i Aplicacions
dc.contributor.author	Llibre Saló, Jaume
dc.contributor.author	Ollé Torner, Mercè
dc.date	2001
dc.identifier.uri	http://hdl.handle.net/2117/1193
dc.language.iso	eng
dc.rights	Attribution-NonCommercial-NoDerivs 2.5 Spain
dc.rights	info:eu-repo/semantics/openAccess
dc.rights	http://creativecommons.org/licenses/by-nc-nd/2.5/es/
dc.subject	Dynamics
dc.subject	Astronomy and astrophysics
dc.subject	Celestial mechanics
dc.subject	Planets and Satellites
dc.subject	Solar system
dc.subject	Partícules (Física nuclear)
dc.subject	Astronomia
dc.subject	Astrofísica
dc.subject	Classificació AMS::70 Mechanics of particles and systems::70F Dynamics of a system of particles, including celestial mechanics
dc.subject	Classificació AMS::85 Astronomy and astrophysics
dc.title	The motion of Saturn coorbital satellites in the restricted three-body problem
dc.type	info:eu-repo/semantics/article
dc.description.abstract	This 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.

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