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.
Attitude control of quadrotor aircraft based on improved expert fuzzy PID
2nd International Conference on Information Technology and Intelligent Control (CITIC 2022) ; 2022 ; Kunming,China
Proc. SPIE ; 12346
2022-09-27
Conference paper
Electronic Resource
English
Attitude control of quadrotor aircraft via nonlinear PID
British Library Online Contents | 2011
|A Fuzzy Theory Based Attitude Control for Takeoff of Quadrotor
Springer Verlag | 2023
|Digital passive attitude and altitude control schemes for quadrotor aircraft
Tema Archive | 2009
|