International audienceThis article deals with the singularly perturbed aircraft minimum time-to-climb problem. First, we introduce a reduced-order problem with affine dynamics with respect to the control and analyze it with the tools from geometric control: maximum principle combined with second order optimality conditions. Then, we compute candidates as minimizers using multiple shooting and homotopy methods for both problems, that we briefly compare numerically. Particular attention is paid to the singular extremals and we discuss about their local optimality
International audienceThe aim of this article is to present algorithms to compute the first conjugat...
A method for the solution of a class of optimal control problems based on a modified steepest descen...
International audienceThis survey article deals with applications of optimal control to aerospace pr...
This article deals with the singularly perturbed aircraft minimum time-to-climb problem. First, we i...
This work concerns the climbing phase of a civil aircraft. The trajectories which minimize the climb...
In this article, we are interested in optimal aircraft trajectories in climbing phase. We consider t...
International audienceIn this article, we are interested in optimal aircraft trajectories in climbin...
Ce travail s’intéresse à la phase de montée d’un aéronef civil. Les trajectoires minimisant le temps...
to appearInternational audienceIn this article, the minimum time and fuel consumption of an aircraft...
The optimization of aircraft trajectories using the theory of singular optimal control is studied in...
Of utmost importance to development of UAVs, is an automatic flight system. Minimum-time maneuvers h...
This paper addresses the time-optimal control problem for a class of control systems which includes...
International audienceAffine control problems arise naturally from controlled mechanical systems. Bu...
Abstract. Necessary conditions for minimax problems with isolated or flat maxima re presented. Some ...
Fuel minimum range cruise of aircraft with high aerodynamic efficiency is considered as an optimal p...
International audienceThe aim of this article is to present algorithms to compute the first conjugat...
A method for the solution of a class of optimal control problems based on a modified steepest descen...
International audienceThis survey article deals with applications of optimal control to aerospace pr...
This article deals with the singularly perturbed aircraft minimum time-to-climb problem. First, we i...
This work concerns the climbing phase of a civil aircraft. The trajectories which minimize the climb...
In this article, we are interested in optimal aircraft trajectories in climbing phase. We consider t...
International audienceIn this article, we are interested in optimal aircraft trajectories in climbin...
Ce travail s’intéresse à la phase de montée d’un aéronef civil. Les trajectoires minimisant le temps...
to appearInternational audienceIn this article, the minimum time and fuel consumption of an aircraft...
The optimization of aircraft trajectories using the theory of singular optimal control is studied in...
Of utmost importance to development of UAVs, is an automatic flight system. Minimum-time maneuvers h...
This paper addresses the time-optimal control problem for a class of control systems which includes...
International audienceAffine control problems arise naturally from controlled mechanical systems. Bu...
Abstract. Necessary conditions for minimax problems with isolated or flat maxima re presented. Some ...
Fuel minimum range cruise of aircraft with high aerodynamic efficiency is considered as an optimal p...
International audienceThe aim of this article is to present algorithms to compute the first conjugat...
A method for the solution of a class of optimal control problems based on a modified steepest descen...
International audienceThis survey article deals with applications of optimal control to aerospace pr...