DocumentCode
2044445
Title
Fuzzy gain scheduling for flight control
Author
Bergsten, P. ; Persson, M. ; Iliev, B.
Author_Institution
Dept. of Technol., Orebro Univ., Sweden
Volume
1
fYear
2000
fDate
2000
Firstpage
271
Abstract
This paper presents a method for design of fuzzy gain scheduled output feedback H∞ controllers for affine Takagi-Sugeno (TS) systems. The method relies on recent developments in design for classical gain scheduling, based on linear matrix inequalities. It is shown how the previous results can be extended to general nonlinear systems that admits a TS fuzzy system approximation. The design method is demonstrated on a nonlinear missile model
Keywords
H∞ control; aerospace control; feedback; fuzzy control; matrix algebra; nonlinear control systems; LMI; T-S fuzzy system approximation; TS fuzzy system approximation; affine Takagi-Sugeno systems; flight control; fuzzy gain scheduled output feedback H∞ controllers; linear matrix inequalities; nonlinear missile model; nonlinear systems; Aerospace control; Control systems; Design methodology; Fuzzy control; Fuzzy systems; Linear matrix inequalities; Missiles; Nonlinear systems; Output feedback; Takagi-Sugeno model;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics Society, 2000. IECON 2000. 26th Annual Confjerence of the IEEE
Conference_Location
Nagoya
Print_ISBN
0-7803-6456-2
Type
conf
DOI
10.1109/IECON.2000.973162
Filename
973162
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