Lunar and J2 perturbations of the metric associated to the averaged orbital transfer
Résumé
In a series of previous article [1,2], we introduced a Riemann-ian metric associated to the energy minimizing orbital transfer with low propulsion. The aim of this article is to study the deformation of this metric due to the standard perturbations in space mechanics, e.g. oblate spheroid shape of the Earth and lunar attraction. Using Hamil-tonian formalism, we describe the effects of the perturbations on the orbital transfers and the deformation of the conjugate and cut loci of the original metric.
Domaines
Optimisation et contrôle [math.OC]
Fichier principal
zermelo.pdf (868.59 Ko)
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hal-zermelo-bonnard-rouot.zip (1.62 Mo)
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| Origine | Fichiers produits par l'(les) auteur(s) |
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| Origine | Fichiers produits par l'(les) auteur(s) |
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