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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

Hindawi Publishing Corporation

Autor: Garcia Taberner, Laura
Masdemont Soler, Josep
Data: 5 juny 2018
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
Accés al document: http://hdl.handle.net/2072/320529
Llenguatge: eng
Editor: Hindawi Publishing Corporation
Drets: Attribution 3.0 Spain
URI Drets: http://creativecommons.org/licenses/by/3.0/es/
Matèria: Algorismes
Algorithms
Títol: An Adaptive Remeshing Procedure for Proximity Maneuvering Spacecraft Formations
Tipus: info:eu-repo/semantics/article
Repositori: Recercat

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