Abstract. The aim of this article is to present the algorithm to compute the first conjugate point along a smooth extremal curve. Under generic assump-tions, the trajectory ceases to be optimal at such a point. An implementation of this algorithm, called cotcot, is available online and based on recent devel-opments in geometric optimal control. It is applied to analyze the averaged optimal transfer of a satellite between elliptic orbits. Introduction. The goal of this article is to summarize the algorithm to compute conjugate points along smooth extremal trajectories. Because of space restriction, we only consider the normal case [4]. The algorithm is implemented in the cotcot code1, and an important application to orbital transfer is given...
International audienceThis article deals with the optimal transfer of a satellite between Keplerian ...
Two interesting and important properties of the conjugate points have been discussed and illustrated...
This article deals with the transfer of a satellite between Keplerian orbits. We study the controlla...
Abstract. The aim of this article is to present the algorithm to compute the first conjugate point a...
International audienceThe aim of this article is to present the algorithm to compute the first conju...
The aim of this article is to present the algorithm to compute the first conjugate point along a smo...
International audienceThe aim of this article is to present algorithms to compute the first conjugat...
The aim of this article is to present algorithms to compute the first conjugate time along a smooth ...
Conjugate point type second order optimality conditions for extremals associated to smooth Hamiltoni...
Cette thèse porte sur l’application de techniques de contrôle optimal et de contrôle géométriques au...
In this thesis we focus on optimal control techniques as well as geometric control techniques applie...
conjugate points. The minimum time control of the Kepler equation is considered. The typ-ical applic...
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
This reference introduces the Matlab package cotcot designed to compute extremals in the case of smo...
This correspondence considers the problem of optimally controlling the thrust steering angle of an i...
International audienceThis article deals with the optimal transfer of a satellite between Keplerian ...
Two interesting and important properties of the conjugate points have been discussed and illustrated...
This article deals with the transfer of a satellite between Keplerian orbits. We study the controlla...
Abstract. The aim of this article is to present the algorithm to compute the first conjugate point a...
International audienceThe aim of this article is to present the algorithm to compute the first conju...
The aim of this article is to present the algorithm to compute the first conjugate point along a smo...
International audienceThe aim of this article is to present algorithms to compute the first conjugat...
The aim of this article is to present algorithms to compute the first conjugate time along a smooth ...
Conjugate point type second order optimality conditions for extremals associated to smooth Hamiltoni...
Cette thèse porte sur l’application de techniques de contrôle optimal et de contrôle géométriques au...
In this thesis we focus on optimal control techniques as well as geometric control techniques applie...
conjugate points. The minimum time control of the Kepler equation is considered. The typ-ical applic...
The optimal control of orbital transfers is considered (problem proposed by the French Space Agency)...
This reference introduces the Matlab package cotcot designed to compute extremals in the case of smo...
This correspondence considers the problem of optimally controlling the thrust steering angle of an i...
International audienceThis article deals with the optimal transfer of a satellite between Keplerian ...
Two interesting and important properties of the conjugate points have been discussed and illustrated...
This article deals with the transfer of a satellite between Keplerian orbits. We study the controlla...