DocumentCode
1893115
Title
The Optimization of Flight Control System Based on an Improved Evolutionary Strategy and Referenced Model
Author
Li, Guangwen ; Jia, Qiuling ; Shi, Jingping
Author_Institution
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an, China
Volume
1
fYear
2009
fDate
10-11 Oct. 2009
Firstpage
918
Lastpage
921
Abstract
The performance and flying quality of the aircraft depend on its flight control system (FCS), and the parameters of the FCS are very difficult to set because the aircraft is a time-varying system and the monotone changing laws of the parameters are required. In this paper, an optimizing method of the parameter of FCS, which is based on an improved evolutionary strategy and referenced model, is proposed. In this method the requirement on the parameter and the flying quality are considered. To validate the effect of this method, a simulation of a kind of aircraft, which covers a big flying envelope, is made. The result shows that parameters gotten by the given fast method are satisfied.
Keywords
aircraft control; evolutionary computation; feedback; optimisation; time-varying systems; aircraft flying quality; aircraft performance; feedback; flight control system optimization; improved evolutionary strategy; monotone changing law; referenced model; time-varying system; Aerospace control; Aircraft; Automation; Educational institutions; Feedback; Genetic mutations; MIMO; Nonlinear systems; Optimization methods; Time varying systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computation Technology and Automation, 2009. ICICTA '09. Second International Conference on
Conference_Location
Changsha, Hunan
Print_ISBN
978-0-7695-3804-4
Type
conf
DOI
10.1109/ICICTA.2009.229
Filename
5287525
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