Design of Aerodynamics Missile Controller Based on Adaptive Fuzzy PID

摘要：

For the Characteristics of missile during flights with nonlinear and coupling and dynamicity, a kind of adaptive fuzzy PID hybrid control strategy is designed, which is used to control the missile attitude motion. In order to more accurately reflect changes in the vicinity of the error rate of zero, the use of fuzzy sets detailed rules for the program control method of fuzzy reasoning adaptive fuzzy PID controller missile flight parameters for online selftuning. Through the simulation results shown that this controller possesses the dynamic response speed, high stability, adaptive anti-jamming ability and good robustness etc.

关键词： Adaptive Control Fuzzy Control PID Control Aerodynamics Missile

作者: Liying Yuan Jiashan Cui Mingyu Pan Yongqi Liu

作者单位: College of Automation Harbin University Of Science And Technology Harbin China

会议类型: 国际会议

会议名称: 2012 International Conference on Measurement,Information and Control(2012测量、信息与控制国际会议 ICMIC2012)

会议地点: 哈尔滨

会议语种:英文

页码: 712-716

在线出版日期: 2012-05-18（万方平台首次上网日期，不代表论文的发表时间）