Anti-windup Nonlinear PID Controller Design and its Application to Winged Missile Control System

被引:3
|
作者
Li Congying [1 ]
Wang Shixing [1 ]
Yue Zhi [1 ]
Yu Jinyong [1 ]
Wang Huijin [1 ]
机构
[1] Naval Aeronaut & Astronaut Univ, Dept Strateg Missel, Yantai 264001, Peoples R China
关键词
Nonlinear PID control; Anti-windup; Gain scheduling; Missile control;
D O I
10.1109/CHICC.2008.4605822
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Nonlinear tracking-differentiator and nonlinear combination were used to improve the behavior of classical PID controller. The result nonlinear PID controller has better adaptability and robustness. An anti-windup compensator was used on the nonlinear PID controller to deal with input constraints in winged missile control system. The use of nonlinear PID controller releases us from complicated work of making gain scheduling table. Characteristic point simulation and full trajectory simulation show validity of the anti-windup NLPID controller. http://ieeexplore.ieee.org/stamp/stamp.jsp?arnumber=4605822
引用
收藏
页码:377 / +
页数:2
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