This article proposes a modal approach to the synthesis of robust systems for optimal stabilization of the program flight path of a UAV under conditions of uncertainty of its state parameters. The synthesis of a modal robust controller is implemented using the principle of guaranteed dynamics, which allows ensuring not only stability, but also the required quality of control. Ref. 14, pic. 1
Les méthodes de synthèse et de validation de lois de pilotage utiliséesdans le milieu industriel aér...
Estimations of the flight vehicles aerodynamic coefficients through the theoretical, numerical, wind...
Unmanned system performance depends heavily on both how the system is planned to be operated and the...
This paper presents a nonlinear robust control design procedure for a micro air vehicle, which uses ...
Stability is not trivial in aerial manipulation tasks because of the dynamical coupling between the ...
Ces travaux de recherche portent sur la synthèse de lois de commande robuste et intelligente pour le...
The article is devoted to the synthesis of robust controllers of supersonic unmanned aerial vehicle ...
The article deals with the support of the guaranteed stability factor of a stabilizing system (SS) f...
This thesis deals with the general problem of controlling rigid-body systems through space, with a s...
A control analysis and design framework is proposed for systems subject to paramet-ric uncertainty. ...
International audienceIn this work, we exploit the recent notion of closed-loop state sensitivity to...
Synthesis of the switching control law for a quadrotor autopilotThe paper deals with the problem of ...
One of the basic problems which have to be solved by Unmanned Automated Vehicles (UAV) involves the ...
The problem of optimal state feedback controller design in terms of quadratic performance ind...
The research work presented in the present PhD thesis focuses on the design and tuning of robust and...
Les méthodes de synthèse et de validation de lois de pilotage utiliséesdans le milieu industriel aér...
Estimations of the flight vehicles aerodynamic coefficients through the theoretical, numerical, wind...
Unmanned system performance depends heavily on both how the system is planned to be operated and the...
This paper presents a nonlinear robust control design procedure for a micro air vehicle, which uses ...
Stability is not trivial in aerial manipulation tasks because of the dynamical coupling between the ...
Ces travaux de recherche portent sur la synthèse de lois de commande robuste et intelligente pour le...
The article is devoted to the synthesis of robust controllers of supersonic unmanned aerial vehicle ...
The article deals with the support of the guaranteed stability factor of a stabilizing system (SS) f...
This thesis deals with the general problem of controlling rigid-body systems through space, with a s...
A control analysis and design framework is proposed for systems subject to paramet-ric uncertainty. ...
International audienceIn this work, we exploit the recent notion of closed-loop state sensitivity to...
Synthesis of the switching control law for a quadrotor autopilotThe paper deals with the problem of ...
One of the basic problems which have to be solved by Unmanned Automated Vehicles (UAV) involves the ...
The problem of optimal state feedback controller design in terms of quadratic performance ind...
The research work presented in the present PhD thesis focuses on the design and tuning of robust and...
Les méthodes de synthèse et de validation de lois de pilotage utiliséesdans le milieu industriel aér...
Estimations of the flight vehicles aerodynamic coefficients through the theoretical, numerical, wind...
Unmanned system performance depends heavily on both how the system is planned to be operated and the...