This thesis discusses the design of an active Fault Tolerant Control (FTC) strategy for improvement of the operational control capability of the safety critical systems. The FTC strategy works in such a way that once a fault is detected by the Fault Detection and Isolation (FDI) unit, a compensation loop is activated for safe recovery. A key feature of the proposed strategy is that the design of the FTC loop is done independently of the nominal control law already in place. For a given application, one can select the appropriate “FTC controller / FDI unit” from the designed set of all admissible FDI/FTC units. The selection is done using performance indicators based on µ-analysis and µg-analysis. Finally, the proposed approach is applied to...
Les systèmes critiques de vol tels que les actionneurs électromécaniques ainsi que les calculateurs ...
Safety is of paramount importance in all transportation systems, but especially in civil aviation. T...
A research initiative within the framework of the Group for Aeronautical Research and Technology in...
Cette thèse porte sur une des préoccupations majeures dans la conception des systèmes automatisés : ...
Cette thèse porte sur une des préoccupations majeures dans la conception des systèmes automatisés : ...
A large transport aircraft simulation benchmark (REconfigurable COntrol for Vehicle Emergency Return...
International audienceIn this article, several schemes related to the field of Fault Detection and I...
Cette thèse fait appel à la commande non linéaire inverse pour faire la synthèse de lois de commande...
This chapter analyses and discusses an active fault-tolerant control (FTC) system for avionic applic...
In this chapter two novel nonlinear aircraft and satellite active fault-tolerant control system stra...
none3This paper addresses the development of a novel active fault tolerant control scheme. The meth...
A large transport aircraft simulation benchmark (REcon¦gurable COn-trol for Vehicle Emergency Return...
A research initiative within the framework of the Group for Aeronautical Research and Technology in...
Major security risks appear with the increase of the number of UAV in the air space. Thus, UAV secur...
The aerospace applications are considered among one of most complex. The non-linear dynamics and cou...
Les systèmes critiques de vol tels que les actionneurs électromécaniques ainsi que les calculateurs ...
Safety is of paramount importance in all transportation systems, but especially in civil aviation. T...
A research initiative within the framework of the Group for Aeronautical Research and Technology in...
Cette thèse porte sur une des préoccupations majeures dans la conception des systèmes automatisés : ...
Cette thèse porte sur une des préoccupations majeures dans la conception des systèmes automatisés : ...
A large transport aircraft simulation benchmark (REconfigurable COntrol for Vehicle Emergency Return...
International audienceIn this article, several schemes related to the field of Fault Detection and I...
Cette thèse fait appel à la commande non linéaire inverse pour faire la synthèse de lois de commande...
This chapter analyses and discusses an active fault-tolerant control (FTC) system for avionic applic...
In this chapter two novel nonlinear aircraft and satellite active fault-tolerant control system stra...
none3This paper addresses the development of a novel active fault tolerant control scheme. The meth...
A large transport aircraft simulation benchmark (REcon¦gurable COn-trol for Vehicle Emergency Return...
A research initiative within the framework of the Group for Aeronautical Research and Technology in...
Major security risks appear with the increase of the number of UAV in the air space. Thus, UAV secur...
The aerospace applications are considered among one of most complex. The non-linear dynamics and cou...
Les systèmes critiques de vol tels que les actionneurs électromécaniques ainsi que les calculateurs ...
Safety is of paramount importance in all transportation systems, but especially in civil aviation. T...
A research initiative within the framework of the Group for Aeronautical Research and Technology in...