Design of Adaptive Fuzzy PID Altitude Control System for Unmanned Aerial Vehicle

• 作 者: SHI Gang YANG Shu-xing JING Ya
• 机 构: School of Aerospace Science and Engineering,Research Institute of Anti-Chemistry
• 出 处: 北京理工大学学报（英文版）
• 发表日期: 2004年期
• 关键词: unmanned aerial vehicle adaptive fuzzy PID altitude control system
• 基金项目: the Ministerial Level Foundation

Based on Matlab/Simulink and Fuzzy Logic toolboxes, the altitude control system is designed and simulated. The validity of conventional PID control method and adaptive fuzzy PID control method is compared. It can be drawn out that the adaptive fuzzy PID control method is superior to the conventional PID in rising time and overshoot etc. The effectiveness of a fuzzy PID controller shows potential application in the future, especially in the presence of model uncertainty or changing dynamics and time-varying parameters.