An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations
dc.contributor.author
dc.date.accessioned
2014-03-24T08:34:02Z
dc.date.available
2014-03-24T08:34:02Z
dc.date.issued
2012
dc.identifier.issn
1024-123X
dc.identifier.uri
dc.description.abstract
We consider a methodology to optimally obtain reconfigurations of spacecraft formations. It is based on the discretization of the time interval in subintervals (called the mesh) and the obtainment of local solutions on them as a result of a variational method. Applied to a libration point orbit scenario, in this work we focus on how to find optimal meshes using an adaptive remeshing procedure and on the determination of the parameter that governs it
dc.format.mimetype
application/pdf
dc.language.iso
eng
dc.publisher
Hindawi Publishing Corporation
dc.relation.isformatof
Reproducció digital del document publicat a: http://dx.doi.org/10.1155/2012/429479
dc.relation.ispartof
Mathematical Problems in Engineering, 2012, p. 429479
dc.relation.ispartofseries
Articles publicats (D-IMA)
dc.rights
Attribution 3.0 Spain
dc.rights.uri
dc.subject
dc.title
An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations
dc.type
info:eu-repo/semantics/article
dc.rights.accessRights
info:eu-repo/semantics/openAccess
dc.embargo.terms
Cap
dc.type.version
info:eu-repo/semantics/publishedVersion
dc.identifier.doi
dc.identifier.idgrec
016198
dc.identifier.eissn
1563-5147