The movement of sixrotor aircraft is introduced in this paper, and its kinetic model is established according to the NewtonEuler equations. The design of fuzzy selfadaptive PID controller is accomplished on the basis of relevant theories of fuzzy control and design process of fuzzy selfadaptive PID controller. Through the analysis of simulation results under Matlab/Simulink simulation system, the controller designed could finish the hover task and achieve the stability control of the aircraft. Finally, control stability of sixrotor aircraft is verified by experiments.
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朱瑛,邹春喜,赵建村.基于模糊自适应PID控制的六旋翼飞行器稳定性控制[J].机床与液压,2016,44(24):39-46. . Stability control for six-rotor aircraft based on fuzzy self-adaptive PID algorithm[J]. Machine Tool & Hydraulics,2016,44(24):39-46