Résumé
This article deals with the optimal transfer of a satellite between Keplerian
orbits using low propulsion and is based on preliminary results of (Geffroy, 1997) where the optimal trajectories are approximated using averaging techniques. The objective is to introduce the geometric framework and to make an analysis of the averaged optimal trajectories in the energy minimization problem, showing in particular the connection with Riemannian problems, with integrable geodesics.
langue originale | Anglais |
---|---|
titre | International Journal of Tomography and Statistics |
Sous-titre | Special Issue on: Control Applications of Optimisation - control and aeronautics, optimal control, control of partial differential equations |
rédacteurs en chef | Delfim TORRES, Emmanuel TRELAT |
Editeur | Indian Society for Development and Environment Research |
Pages | 20-25 |
Nombre de pages | 6 |
Volume | 5:W07 |
Etat de la publication | Publié - 2007 |