DocumentCode
2650945
Title
Static output feedback for aeroengine control system
Author
Hao, Binbin ; Qu, Tao
Author_Institution
AVIC shenyang engine design & Res. Inst., Shenyang, China
fYear
2012
fDate
23-25 May 2012
Firstpage
4233
Lastpage
4236
Abstract
This paper considers the static output feedback control synthesis problem of aeroengine system. By introducing a slack variable for separating system matrix and Lyapunov matrix, more relaxed sufficient conditions for designing static output feedback controller are given in terms of solutions to a set of linear matrix inequalities. Simulation illustrates that the proposed methods for aeroengine systems can achieve good performance.
Keywords
Lyapunov matrix equations; aerospace engines; control system synthesis; feedback; linear matrix inequalities; Lyapunov matrix; aeroengine control system; linear matrix inequalities; separating system matrix; slack variable; static output feedback control synthesis problem; Control theory; Linear matrix inequalities; Output feedback; Robustness; Symmetric matrices; TV; SISO control; aeroengine; linear matrix inequalities; multivariable control; robust H2 control; static output feedback;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2012 24th Chinese
Conference_Location
Taiyuan
Print_ISBN
978-1-4577-2073-4
Type
conf
DOI
10.1109/CCDC.2012.6243118
Filename
6243118
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