Flying control system simulation modeling using simulink

被引:0
作者
Li, HG [1 ]
Feng, ZS [1 ]
Gu, HQ [1 ]
Chen, JH [1 ]
机构
[1] Mech Engn Coll, Dept Missile Engn, Shijiazhuang, Peoples R China
来源
PROCEEDINGS OF THE 4TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION, VOLS 1-4 | 2002年
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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.
引用
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页码:147 / 150
页数:4
相关论文
共 7 条
[1]  
ATHERTON DP, 1994, P ADV CONTR ENG JAP
[2]   Object oriented analysis, modeling, and simulation of a notional air defense system [J].
Barcio, BT ;
Ramaswamy, S ;
Macfadzean, R ;
Barber, KS .
SIMULATION, 1996, 66 (01) :5-21
[3]  
Kahaner D., 1989, Numerical Methods and Software
[4]  
Kwon OB, 1996, SIMULATION, V66, P93, DOI 10.1177/003754979606600206
[5]  
*MATH WORKS, 1995, MATLAB VERS 4 2 US G
[6]   Evaluation of missile guidance and control systems on a personal computer [J].
Rodriguez, AA ;
Sonne, ML .
SIMULATION, 1997, 68 (06) :363-376
[7]   A SUBOPTIMAL REDUCTION ALGORITHM FOR LINEAR-SYSTEMS WITH A TIME-DELAY [J].
XUE, DY ;
ATHERTON, DP .
INTERNATIONAL JOURNAL OF CONTROL, 1994, 60 (02) :181-196