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Design of UAV Attitude Controller Based on Fuzzy PID
Received date: 2014-02-10
Online published: 2025-05-26
The design of adaptive fuzzy PID UAV attitude control uses common PID control method and fuzzy control algorithm, since the membership function is over dependent on expert experience; genetic algorithm is used to optimize the membership function, the optimal control effect. The dynamic performance and robustness of the controller are greatly improved compared with traditional attitude controller, which is proved by simulation.
Key words: fuzzy PID; UAV; attitude controller; optimization of membership function
CHEN Peng , DUAN Fengyang , ZHANG Qingjie , ZHENG Zhicheng , XIAO Wei . Design of UAV Attitude Controller Based on Fuzzy PID[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(1) : 9 -11,18 . DOI: 10.15892/j.cnki.djzdxb.2015.01.003
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