Fuzzy-PID Based Approach to Design of Attitude Control for Cruise Munition
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.
Peichun XIAO Yong HE
School of Mechanical Engineering, Nanjing University of Science & Technology.Jiangsu, China
国际会议
The 4th International Conference on Mechanical Engineering and Mechanics(第四届国际机械工程与力学会议)
苏州
英文
285-290
2011-08-11（万方平台首次上网日期，不代表论文的发表时间）