DocumentCode :
3469412
Title :
Discrete time H control laws for a high performance helicopter
Author :
Walker, D. ; Postlethwaite, I.
Author_Institution :
Dept. of Eng., Leicester Univ., UK
fYear :
1991
fDate :
11-13 Dec 1991
Firstpage :
128
Abstract :
An application of the 2 Ricatti equation theory for discrete-time H optimization is presented. Two helicopter flight control laws are designed. The first design is based on a normalized coprime factor stabilization. The second uses a standard 2-block sensitivity and robustness formulation. The designs presented here are novel in that the problem is posed from the outset as a discrete-time (DT) problem which is solved using recent game-theoretic formulae for DT H optimization. It is shown that by suitable choice of weighting functions it is possible to obtain directly DT controllers that give good levels of performance and robustness
Keywords :
aircraft control; control system synthesis; discrete time systems; game theory; helicopters; optimal control; optimisation; stability; 2-block sensitivity; Ricatti equation; aircraft control; control system synthesis; discrete-time H optimization; helicopter; normalized coprime factor stabilization; optimal control; robustness; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Design optimization; Equations; H infinity control; Helicopters; Open loop systems; Riccati equations; Robust control; Robust stability; Robustness;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 1991., Proceedings of the 30th IEEE Conference on
Conference_Location :
Brighton
Print_ISBN :
0-7803-0450-0
Type :
conf
DOI :
10.1109/CDC.1991.261269
Filename :
261269
Link To Document :
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