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An adaptive remeshing procedure for proximity maneuvering spacecraft formations

Autor
Garcia-Taberner, L.; Masdemont, J.J.
Tipus d'activitat
Article en revista
Revista
Mathematical problems in engineering
Data de publicació
2012
Volum
2012
Pàgina inicial
1
Pàgina final
14
DOI
https://doi.org/10.1155/2012/429479 Obrir en finestra nova
Repositori
http://hdl.handle.net/2117/16528 Obrir en finestra nova
URL
http://www.hindawi.com/journals/mpe/2012/429479/ Obrir en finestra nova
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.
Citació
Garcia-Taberner, L.; Masdemont, J.J. An adaptive remeshing procedure for proximity maneuvering spacecraft formations. "Mathematical problems in engineering", 2012, vol. 2012, p. 1-14.
Grup de recerca
SD - Sistemes Dinàmics de la UPC

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