Payload optimization for multi-stage launchers using HJB approach and application to a SSO mission

Abstract : This paper deals with a payload optimization problem for three-stage space launcher. The mission of the launch vehicle is to put the payload on a sun-synchronous (SSO) orbit. The considered flight sequence includes two boosts. The first one steers the launcher to a transfer orbit. Then, after a ballistic flight, a second boost is used to perform the orbit transfer manoeuvre to inject the payload to the targeted SSO orbit. The optimization method presented here is based on the Hamilton-Jacobi-Bellman (HJB) approach for hybrid dynamical systems.
Type de document :
Communication dans un congrès
The 20th IFAC World Congress , Jul 2017, Toulouse, France. 2017, 〈10.1016/j.ifacol.2017.08.647〉
Liste complète des métadonnées

Littérature citée [16 références]  Voir  Masquer  Télécharger

https://hal-ensta.archives-ouvertes.fr/hal-01598665
Contributeur : Hasnaa Zidani <>
Soumis le : vendredi 29 septembre 2017 - 18:42:51
Dernière modification le : vendredi 31 août 2018 - 09:06:03
Document(s) archivé(s) le : samedi 30 décembre 2017 - 15:50:23

Fichier

Bou-Bok-Des-Zidani.pdf
Fichiers produits par l'(les) auteur(s)

Identifiants

Citation

Olivier Bokanowski, Eric Bourgeois, Anna Desilles, Hasnaa Zidani. Payload optimization for multi-stage launchers using HJB approach and application to a SSO mission. The 20th IFAC World Congress , Jul 2017, Toulouse, France. 2017, 〈10.1016/j.ifacol.2017.08.647〉. 〈hal-01598665〉

Partager

Métriques

Consultations de la notice

328

Téléchargements de fichiers

60