This thesis contribute to the optimal time study of control-affine systems. These problems arise naturally from physics, and contains, for instance, mechanical systems. We tackle the study of their singularities, while minimizing the final time, meaning the time on which the aim is reached. We give a precise study of the extremal flow, for mechanical systems, for starter, and then, in general. This leads to the knowledge of the flow regularity: it is smooth on a stratification around the singular set. We then apply those results to mechanical systems, and orbit transfer problems, with two and three bodies, giving an upper bound to the number of singularities occurring during a transfer. We then change our viewpoint to study the optimality o...
The technique of averaging is an effective way to simplify optimal low-thrust satellite transfers in...
This work concerns the climbing phase of a civil aircraft. The trajectories which minimize the climb...
L'objet principal de cette thèse est l'application de méthodes nouvelles inspirées de l'analyse non-...
Cette thèse contribue à l'étude en temps minimal des systèmes de contrôle affines. Les systèmes dépe...
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
International audienceAffine control problems arise naturally from controlled mechanical systems. Bu...
International audienceAffine control problems arise naturally from controlled mechanical systems. Bu...
International audienceThe case of time minimization for affine control systems with control on the d...
Conjugate point type second order optimality conditions for extremals associated to smooth Hamiltoni...
We deal with a problem from celestial mechanics, namely the minimum-time orbit transfer towards a ge...
conjugate points. The minimum time control of the Kepler equation is considered. The typ-ical applic...
The minimum time control of the Kepler equation is considered. The typical application is the transf...
Jury : F. H. Clarke, M.-O. Czarnecki, J.-B. Hiriart-Urruty, L. Rifford, R. Stern, P. WolenskiThe mai...
The technique of averaging is an effective way to simplify optimal low-thrust satellite transfers in...
This work concerns the climbing phase of a civil aircraft. The trajectories which minimize the climb...
L'objet principal de cette thèse est l'application de méthodes nouvelles inspirées de l'analyse non-...
Cette thèse contribue à l'étude en temps minimal des systèmes de contrôle affines. Les systèmes dépe...
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
International audienceAffine control problems arise naturally from controlled mechanical systems. Bu...
International audienceAffine control problems arise naturally from controlled mechanical systems. Bu...
International audienceThe case of time minimization for affine control systems with control on the d...
Conjugate point type second order optimality conditions for extremals associated to smooth Hamiltoni...
We deal with a problem from celestial mechanics, namely the minimum-time orbit transfer towards a ge...
conjugate points. The minimum time control of the Kepler equation is considered. The typ-ical applic...
The minimum time control of the Kepler equation is considered. The typical application is the transf...
Jury : F. H. Clarke, M.-O. Czarnecki, J.-B. Hiriart-Urruty, L. Rifford, R. Stern, P. WolenskiThe mai...
The technique of averaging is an effective way to simplify optimal low-thrust satellite transfers in...
This work concerns the climbing phase of a civil aircraft. The trajectories which minimize the climb...
L'objet principal de cette thèse est l'application de méthodes nouvelles inspirées de l'analyse non-...