Dynamics and mission design near libration points, advanced methods for triangular points

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To access the full text documents, please follow this link: http://hdl.handle.net/2117/1214

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	Gómez, Gerard
dc.contributor.author	Jorba, Angel
dc.contributor.author	Masdemont Soler, Josep
dc.contributor.author	Simó Torres, Carlos
dc.date	2000
dc.identifier.uri	http://hdl.handle.net/2117/1214
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	Differentiable dynamical systems
dc.subject	Dynamics
dc.subject	Orbital mechanics
dc.subject	equilateral points
dc.subject	Earth-Moon system
dc.subject	Sistemes dinàmics diferenciables
dc.subject	Teoria ergòdica
dc.subject	Partícules (Física nuclear)
dc.subject	Òrbites
dc.subject	Mecànica celest
dc.subject	Classificació AMS::37 Dynamical systems and ergodic theory::37N Applications
dc.subject	Classificació AMS::70 Mechanics of particles and systems::70F Dynamics of a system of particles, including celestial mechanics
dc.subject	Classificació AMS::70 Mechanics of particles and systems::70M20 Orbital mechanics
dc.title	Dynamics and mission design near libration points, advanced methods for triangular points
dc.type	info:eu-repo/semantics/article
dc.description.abstract	The final objective of this work is to understand, analyze and compute the kinds of motion that appear on a vicinity (may be a large vicinity) of the geometrically defined equilateral points of the Earth-Moon system, as a source of possible nominal orbits for future space missions.

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