The report describes the work done on Design of Stability Augmentation Systems for modern aircraft using Vector Optimisation T.echniques Parameter Space Mapping and Robust Output Observer theory have been used to determine the initial values for the controller parameters prior to optimisation . Typical results are also presented to substantiate the design procedure
This thesis addresses the application issues raised implementing flight control designs derived from...
In this paper the problem of integrated design and control for a civil blended wing-body aircraft is...
Designing a flight control system for an aircraft is a multifaceted task which has to take many requ...
A multi-model multi-criteria vector optimisation technique based on the minimisation of the Kreissel...
The report describes the development of a flight control system synthesis software based on a multi-...
A survey of the stability analysis techniques for automatically controlled aircraft is presented. Th...
Development of new control configured flight vehicles has introduced challenging problems in both th...
The handling qualities of an aircraft have always been a crucial field of study, being chiefly conce...
This research focused on incorporating stability and control into a multidisciplinary de- sign optim...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...
Flight control system design typically involves hardware and software development, requiring the def...
THESIS 8104This thesis develops for the first time a general approach to the design of control syste...
Theoretical development is reported for the parameter optimization design technique needed for digit...
Afin d'améliorer les performances et l'efficacité des avions civils, les développements actuels sont...
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
This thesis addresses the application issues raised implementing flight control designs derived from...
In this paper the problem of integrated design and control for a civil blended wing-body aircraft is...
Designing a flight control system for an aircraft is a multifaceted task which has to take many requ...
A multi-model multi-criteria vector optimisation technique based on the minimisation of the Kreissel...
The report describes the development of a flight control system synthesis software based on a multi-...
A survey of the stability analysis techniques for automatically controlled aircraft is presented. Th...
Development of new control configured flight vehicles has introduced challenging problems in both th...
The handling qualities of an aircraft have always been a crucial field of study, being chiefly conce...
This research focused on incorporating stability and control into a multidisciplinary de- sign optim...
This thesis presents one of the first applications of H∞-optimization to the design of controllers f...
Flight control system design typically involves hardware and software development, requiring the def...
THESIS 8104This thesis develops for the first time a general approach to the design of control syste...
Theoretical development is reported for the parameter optimization design technique needed for digit...
Afin d'améliorer les performances et l'efficacité des avions civils, les développements actuels sont...
International audiencePiloting a helicopter is a demanding task for human operators: autopilots have...
This thesis addresses the application issues raised implementing flight control designs derived from...
In this paper the problem of integrated design and control for a civil blended wing-body aircraft is...
Designing a flight control system for an aircraft is a multifaceted task which has to take many requ...