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dc.contributor.authorMasdemont Soler, Josep
dc.contributor.authorGarcía Taberner, Laura
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Matemàtica Aplicada I
dc.date.accessioned2011-02-28T10:36:03Z
dc.date.available2011-02-28T10:36:03Z
dc.date.created2010
dc.date.issued2010
dc.identifier.citationMasdemont, J.J.; Garcia-Taberner, L. Spacecraft formations reconfiguration using finite element methodology with adaptive remeshing. A: Conference on Nonlinear Science and Complexity. "3rd Conference on Nonlinear Science and Complexity NCS10". Ankara: 2010.
dc.identifier.urihttp://hdl.handle.net/2117/11562
dc.description.abstractWe present a methodology to compute trajectories for formation °ying recon¯g- uration problems using a methodology based on ¯nite elements: FEFF (Finite Elements for Formation Flying). In this paper we center ourselves on the obtention of optimal meshes using adaptive remeshing. As an application we show how adaptive remeshing is applied to two kinds of recon¯gurations: a class where is known that a bang-bang control is the optimal solution and another class where bang-bang would end up in collision. In the ¯rst case the methodology tends to the optimal bang-bang, while in the second one, tends to a low thrust control. Finally, we update the trajectories obtained with FEFF and adaptive remeshing to the JPL-ephemeris model to test the reliability of the methodology.
dc.format.extent1 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.subject.lcshAstrodynamics
dc.titleSpacecraft formations reconfiguration using finite element methodology with adaptive remeshing
dc.typeConference report
dc.subject.lemacAstrodinàmica
dc.contributor.groupUniversitat Politècnica de Catalunya. EGSA - Equacions Diferencials, Geometria, Sistemes Dinàmics i de Control, i Aplicacions
dc.relation.publisherversionhttp://nsc10.cankaya.edu.tr/proceedings/PAPERS/Symp5-Celestial%20Mechanics%20and%20Dynamical%20Astronomy%20Methods%20and%20Applications/Paper52.pdf
dc.rights.accessOpen Access
drac.iddocument5238842
dc.description.versionPostprint (published version)
upcommons.citation.authorMasdemont, J.J.; Garcia-Taberner, L.
upcommons.citation.contributorConference on Nonlinear Science and Complexity
upcommons.citation.pubplaceAnkara
upcommons.citation.publishedtrue
upcommons.citation.publicationName3rd Conference on Nonlinear Science and Complexity NCS10


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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