Fixed Structure Flight Control Law Design Based on Genetic Algorithm

Author

Qing-tang, Feng ; Zhi-hong, Jiang ; Ji-hong, Zhu ; Shi-qian, Liu

Author_Institution

State Key Lab. of Intelligent Technol. & Syst., Tsinghua Univ., Beijing

Volume

1

fYear

2006

fDate

4-6 Oct. 2006

Firstpage

659

Lastpage

662

Abstract

The development of flight control systems using classical control techniques is a costly and time-consuming process. This paper shows how to use genetic algorithm (GA) and modern control techniques to determine the control parameters of the flight control law within the classical structure. An example of designing longitudinal flight control law with the proposed method is presented. The designed flight control law be simulated on a 6 degree-of-freedom nonlinear model of the aircraft

Keywords

aerospace control; control system synthesis; genetic algorithms; performance index; flight control law design; genetic algorithm; quadratic performance index; Aerospace control; Aerospace engineering; Aircraft propulsion; Algorithm design and analysis; Control systems; Elevators; Frequency measurement; Genetic algorithms; Q measurement; Systems engineering and theory; flight control law; genetic algorithm; quadratic performance index;

fLanguage

English

Publisher

ieee

Conference_Titel

Computational Engineering in Systems Applications, IMACS Multiconference on

Conference_Location

Beijing

Print_ISBN

7-302-13922-9

Electronic_ISBN

7-900718-14-1

Type

conf

DOI

10.1109/CESA.2006.4281735

Filename

4281735