DocumentCode
2022391
Title
Flying control system simulation modeling using Simulink
Author
Hongru, Li ; Zhensheng, Feng ; Hongqiang, Gu ; Jianhui, Chen
Author_Institution
Dept. of Missile Eng., Mech. Eng. Coll., Shijiazhuang, China
Volume
1
fYear
2002
fDate
2002
Firstpage
147
Abstract
A subsection modeling and dynamic switching method Is developed. First, the system is studied and the mathematical models for every time-period are set up. Then, the simulation models for every time-period are established. Finally, a m-function is designed which makes the simulation models for every time-period be linked and the system states be continuous. This method is applied to the simulation modeling of a flying control system, the simulation speed is greatly accelerated.
Keywords
aerospace computing; aircraft control; control engineering computing; digital simulation; engineering graphics; Simulink; dynamic switching method; flying control system simulation modeling; m-function; subsection modeling method; Aerodynamics; Atmosphere; Computational modeling; Control system synthesis; Fuels; Large-scale systems; Mathematical model; Power system modeling; Vehicle dynamics; Vibration control;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2002. Proceedings of the 4th World Congress on
Print_ISBN
0-7803-7268-9
Type
conf
DOI
10.1109/WCICA.2002.1022087
Filename
1022087
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