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
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