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
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;
Conference_Titel :
Intelligent Control and Automation, 2002. Proceedings of the 4th World Congress on
Print_ISBN :
0-7803-7268-9
DOI :
10.1109/WCICA.2002.1022087