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An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations

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

Mathematical Problems in Engineering, 2012, p. 429479

Hindawi Publishing Corporation

Autor: Garcia Taberner, Laura
Masdemont Soler, Josep
Data: 2012
Resum: 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
Format: application/pdf
ISSN: 1024-123X (versi贸 paper)
1563-5147 (versi贸 electr貌nica)
Acc茅s al document: http://hdl.handle.net/10256/8975
Llenguatge: eng
Editor: Hindawi Publishing Corporation
Col路lecci贸: Reproducci贸 digital del document publicat a: http://dx.doi.org/10.1155/2012/429479
Articles publicats (D-IMA)
脡s part de: Mathematical Problems in Engineering, 2012, p. 429479
Drets: Attribution 3.0 Spain
URI Drets: http://creativecommons.org/licenses/by/3.0/es/
Mat猫ria: Algorismes
Algorithms
T铆tol: An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations
Tipus: info:eu-repo/semantics/article
Repositori: DUGiDocs

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