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