Design of aerodynamics missile controller based on adaptive fuzzy PID

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 self-tuning. Through the simulation results shown that this controller possesses the dynamic response speed, high stability, adaptive anti-jamming ability and good robustness etc.