DocumentCode :
700486
Title :
Optimal H-infinity design of a control system for the angle of attack
Author :
Stoica, A.
Author_Institution :
Dept. of Aerosp. Eng., Polytech. Univ. of Bucharest, Bucharest, Romania
fYear :
1997
fDate :
1-7 July 1997
Firstpage :
337
Lastpage :
342
Abstract :
The paper presents a method for the design of a control system for the angle of attack of a fighter based on a model-matching technique. The H problem to which the model-matching problem reduces has been solved by using an optimal approach described in Appendix. The paper includes a comparison of different performances of the control system obtained by using this optimal method with the ones given by the suboptimal H design, showing that the optimal approach offers considerable advantages.
Keywords :
H control; aerospace control; control system synthesis; military aircraft; suboptimal control; H problem; control system design; fighter; fighter aircraft; flight control system; model-matching technique; optimal H-infinity design; suboptimal H design; Aerospace control; Attenuation; Control systems; Robustness; Stability criteria; Uncertainty; Aerospace; H; Numerical methods;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 1997 European
Conference_Location :
Brussels
Print_ISBN :
978-3-9524269-0-6
Type :
conf
Filename :
7082116
Link To Document :
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