The zero, minimum and maximum relative radial accelerations along a family of periodic orbits around L4 in the Earth-Moon system

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To access the full text documents, please follow this link: http://hdl.handle.net/2117/17710

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	Salazar, F.J.T.
dc.contributor.author	Masdemont Soler, Josep
dc.contributor.author	Gómez Muntané, Gerard
dc.contributor.author	Macau, E.E.N.
dc.contributor.author	Winter, O.C.
dc.date	2012
dc.identifier.citation	Salazar, F.J.T. [et al.]. The zero, minimum and maximum relative radial accelerations along a family of periodic orbits around L4 in the Earth-Moon system. A: Workshop de Computaçao Aplicada. "Textos web". Sao Jose dos Campos: 2012, p. 1-10.
dc.identifier.uri	http://hdl.handle.net/2117/17710
dc.language.iso	eng
dc.rights	Attribution-NonCommercial-NoDerivs 3.0 Spain
dc.rights	info:eu-repo/semantics/openAccess
dc.rights	http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject	Àrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciències
dc.subject	Mecànica celest
dc.title	The zero, minimum and maximum relative radial accelerations along a family of periodic orbits around L4 in the Earth-Moon system
dc.type	info:eu-repo/semantics/publishedVersion
dc.type	info:eu-repo/semantics/conferenceObject
dc.description.abstract	Constellations of satellites, Zero relative radial acceleration, Earth-Moon.
dc.description.abstract	Assume a constellations of satellites flighting close a given nominal trajectory around L4 or L5 in the Earth-Moon system in such a way that there is freedom in the selection of the geometry of the constellation. We are interested in to avoid large variations of the mutual distance between the spacecrafts. In this case, the possible existence of regions of zero relative radial acceleration with respect to the nominal trajectory will prevent from the expansion or contraction of the constellation. The goal of this paper is the study of theses regions.

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