Title :
Design of flight control system for an aeroelastic aircraft
Author :
Kubica, F. ; Livet, T.
Author_Institution :
Aircraft Div., Aerospatiale, Toulouse, France
Abstract :
The evolution of modern day aircraft increases the interaction between aeroelastic dynamics and control laws, known as aeroservoelasticity. An integrated flight control system without structural filters is proposed in order to achieve good handling qualities and increase structural mode damping. In the first step sensor and actuator location is studied, and in a second step the use of the linear quadratic regulator with output feedback for the synthesis of the control law
Keywords :
aircraft control; control system synthesis; elasticity; feedback; linear quadratic control; actuator location; aeroelastic aircraft; aeroservoelasticity; integrated flight control system design; linear quadratic regulator; output feedback; sensor location; structural mode damping; Aircraft control; Linear-quadratic control; Mechanical factors; Output feedback;
Conference_Titel :
Control Applications, 1994., Proceedings of the Third IEEE Conference on
Conference_Location :
Glasgow
Print_ISBN :
0-7803-1872-2
DOI :
10.1109/CCA.1994.381445
