DocumentCode
1585551
Title
Design of three-axis flight simulator controller based on genetic algorithm
Author
Xu, Hongze ; Jin, Ling
Author_Institution
Dept. of Autom., Beijing Jiaotong Univ., China
Volume
6
fYear
2004
Firstpage
5430
Abstract
The control system of three-axis flight simulator was required to have excellent dynamic tracing performance as well as fine noise-restrained property because the coupling in the frames of the flight simulator and the indeterminate time-invariant disturber in the hydraulic pressure system exists. Based on the characteristic of three-axis flight simulator, two-degree-of-freedom PID controller for outer-frame of flight simulator was designed. This type of controller had the capability of tracing target value as well as restraining noise. In addition, the outer-frame controller parameters were set based on improved genetic algorithm. Simulation results show the effectiveness of the controller. At the same time, the controller, which was designed based on the nominal model, is used on the other model. Simulation results show that the controller has the property of robustness.
Keywords
aerospace simulation; control system synthesis; genetic algorithms; hydraulic systems; position control; robust control; three-term control; PID controller; genetic algorithm; hydraulic pressure system; indeterminate time-invariant disturber; outer-frame controller parameters; robust control; three-axis flight simulator controller; Aerospace simulation; Algorithm design and analysis; Control system synthesis; Genetic algorithms; Pressure control; Three-term control;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2004. WCICA 2004. Fifth World Congress on
Print_ISBN
0-7803-8273-0
Type
conf
DOI
10.1109/WCICA.2004.1343768
Filename
1343768
Link To Document