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dc.contributor.authorGarcía Taberner, Laura
dc.contributor.authorMasdemont Soler, Josep
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I
dc.date.accessioned2010-08-12T10:27:52Z
dc.date.available2010-08-12T10:27:52Z
dc.date.created2009
dc.date.issued2009
dc.identifier.citationGarcia-Taberner, L.; Masdemont, J.J. Reconfiguration of spacecraft formations in the vicinity of libration points. A: International Astronautical Congress. "60th International Astronautical Congress". Daejeon: 2009, p. 1-9.
dc.identifier.isbn1995-6258 (ISSN)
dc.identifier.urihttp://hdl.handle.net/2117/8908
dc.description.abstractFormation °ying is an important concept demanding reliable and accurate techniques for the recon¯gura- tion or the deployment of the spacecraft. This paper is a contribution to these set of techniques considering a ¯nite element approach. The formulation allows to compute proximity maneuvers for the spacecraft and, at the same time, to incorporate optimal control techniques which include collision avoidance or many other types of constraints. The computations have been carried out about libration point orbits of the Sun-Earth system and using linearized equations about a nonlinear nominal base orbit. The trajectories obtained for this model have been corrected considering a full nonlinear model (JPL-ephemeris). Also random errors have been added to the nominal recon¯guration maneuvers to simulate small thrust errors. The presented methodology proves to be robust in both the computation of the nominal recon¯guration maneuvers and in the correction of the perturbations.
dc.format.extent9 p.
dc.language.isoeng
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Matemàtiques i estadística
dc.titleReconfiguration of spacecraft formations in the vicinity of libration points
dc.typeConference report
dc.subject.lemacÒrbites
dc.contributor.groupUniversitat Politècnica de Catalunya. EGSA - Equacions Diferencials, Geometria, Sistemes Dinàmics i de Control, i Aplicacions
dc.relation.publisherversionhttp://www.iafastro.net/download/congress/IAC-09/DVD/full/IAC-09/C1/5/manuscripts/IAC-09.C1.5.8.pdf
dc.rights.accessOpen Access
drac.iddocument2634321
dc.description.versionPostprint (published version)
upcommons.citation.authorGarcia-Taberner, L.; Masdemont, J.J.
upcommons.citation.contributorInternational Astronautical Congress
upcommons.citation.pubplaceDaejeon
upcommons.citation.publishedtrue
upcommons.citation.publicationName60th International Astronautical Congress
upcommons.citation.startingPage1
upcommons.citation.endingPage9


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Except where otherwise noted, content on this work is licensed under a Creative Commons license: Attribution-NonCommercial-NoDerivs 3.0 Spain