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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

Author: Garcia Taberner, Laura
Masdemont Soler, Josep
Date: 2012
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
Format: application/pdf
ISSN: 1024-123X (versió paper)
1563-5147 (versió electrònica)
Document access: http://hdl.handle.net/10256/8975
Language: eng
Publisher: Hindawi Publishing Corporation
Collection: Reproducció digital del document publicat a: http://dx.doi.org/10.1155/2012/429479
Articles publicats (D-IMA)
Is part of: Mathematical Problems in Engineering, 2012, p. 429479
Rights: Attribution 3.0 Spain
Rights URI: http://creativecommons.org/licenses/by/3.0/es/
Subject: Algorismes
Algorithms
Title: An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations
Type: info:eu-repo/semantics/article
Repository: DUGiDocs

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