DocumentCode :
300463
Title :
Robustness analysis of controllers designed for active flutter suppression
Author :
Toker, Onur ; Özbay, Hitay
Author_Institution :
Dept. of Electr. Eng., Ohio State Univ., Columbus, OH, USA
Volume :
1
fYear :
1995
fDate :
21-23 Jun 1995
Firstpage :
182
Abstract :
In this paper different controller design techniques are studied for a linear model of a two dimensional thin airfoil. The controller design methods considered here are, LQG, gap metric optimization, loop-shaping via weighted gap optimization, mixed sensitivity minimization via H design and robust performance optimization via μ synthesis. The results of flutter speed analysis are compared for each of these controllers. Also, the effects of unmodelled delays on closed loop stability are discussed with simulation results
Keywords :
closed loop systems; control system synthesis; linear quadratic control; multidimensional systems; optimisation; robust control; stability; μ synthesis; 2D thin airfoil; H design; active flutter suppression; closed loop stability; flutter speed analysis; gap metric optimization; linear model; linear quadratic control; loop-shaping; mixed sensitivity minimization; robustness analysis; unmodelled delays; Actuators; Automotive components; Closed loop systems; Delay effects; Design methodology; Design optimization; Mathematical model; Minimization methods; Robust control; Robust stability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, Proceedings of the 1995
Conference_Location :
Seattle, WA
Print_ISBN :
0-7803-2445-5
Type :
conf
DOI :
10.1109/ACC.1995.529233
Filename :
529233
Link To Document :
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