Quadrotor aircraft system is strongly coupled and underactuated, which is a nonlinear flight control model. It is easy to b e affected by system uncertainty and external disturbance during flight. Therefore, an improved fuzzy PID control with e xpert control method is proposed. After establishing the mathematical model of the quadrotor aircraft, the fuzzy PID cont rol method is optimized and improved, and the fuzzy control is optimized by using expert rules and experience. Through Matlab/Simulink simulation comparison, the results show that the proposed control algorithm can optimize the control ef fect of the quadrotor aircraft.


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    Title :

    Attitude control of quadrotor aircraft based on improved expert fuzzy PID


    Contributors:
    Shen, Chao (author) / Li, Yuan (author)

    Conference:

    2nd International Conference on Information Technology and Intelligent Control (CITIC 2022) ; 2022 ; Kunming,China


    Published in:

    Proc. SPIE ; 12346


    Publication date :

    2022-09-27





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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