Fuzzy-PID Based Approach to Design of Attitude Control for Cruise Munition

摘要

The attitude control is the base of autonomic flight control for cruise munition, the design of attitude flight controller determines the autonomic flight quality. To get an easy and efficient flight control method for cruise munition, this paper introduces fuzzy-PID control approach and proposes a fuzzy-PID based flight controller which applies the fuzzy-PID approach in the pitching attitude control loop. The stimulate results clearly show that, compared with the traditional PID controller, this fuzzy-PID based controller has better reliability, robustness and adaptability.