Item
Garcia Taberner, Laura
Masdemont Soler, Josep |
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2012 | |
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 | |
application/pdf | |
1024-123X (versi贸 paper) 1563-5147 (versi贸 electr貌nica) |
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http://hdl.handle.net/10256/8975 | |
eng | |
Hindawi Publishing Corporation | |
Reproducci贸 digital del document publicat a: http://dx.doi.org/10.1155/2012/429479 Articles publicats (D-IMA) |
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Mathematical Problems in Engineering, 2012, p. 429479 | |
Attribution 3.0 Spain | |
http://creativecommons.org/licenses/by/3.0/es/ | |
Algorismes
Algorithms |
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An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations | |
info:eu-repo/semantics/article | |
DUGiDocs |