Title :
Optimal output feedback control: a multi-model approach
Author_Institution :
Inst. for Robotics & Syst. Dynamics, German Aerosp. Res. Establ., Wessling, Germany
Abstract :
In this paper we describe a computational approach to the optimal output feedback control of multi-model systems by means of a unique constant output feedback matrix. Extension of the method to output feedback control of multi-model periodic systems is also presented. The power of the proposed approach is illustrated by the simultaneous stabilization and optimization of a helicopter multi-model
Keywords :
control system CAD; feedback; optimal control; optimisation; periodic control; stability; time-varying systems; computational approach; helicopter multi-model; multi-model approach; multimodel periodic systems; optimal output feedback control; unique constant output feedback matrix; Aerodynamics; Aerospace control; Control systems; Helicopters; Linear matrix inequalities; Optimal control; Output feedback; Performance analysis; Robots; Tin;
Conference_Titel :
Computer-Aided Control System Design, 1996., Proceedings of the 1996 IEEE International Symposium on
Conference_Location :
Dearborn, MI
Print_ISBN :
0-7803-3032-3
DOI :
10.1109/CACSD.1996.555313
