scholarly journals Design of UAV yaw Angle controller based on variable domain fuzzy PID

2021 ◽  
Vol 1754 (1) ◽  
pp. 012112
Author(s):  
Wang Ning ◽  
Li Zhe ◽  
Liang Xiaolong ◽  
Zhang Jiaqiang
Keyword(s):  
2021 ◽  
Author(s):  
Yixu Wang ◽  
Xiaoqing Guan ◽  
Tao Hu ◽  
Ziang Zhang ◽  
You Wang ◽  
...  

2021 ◽  
Vol 284 ◽  
pp. 04008
Author(s):  
Dongwen Yan

Aiming at the problem of low control efficiency of small stable platform due to frame coupling, an intelligent control algorithm (fuzzy-PID) combining fuzzy controller with traditional PID is designed. The fuzzy PID controller is added to the position closed loop of the stable platform control system, and the motor position signal is collected and analyzed. Compared with the traditional PID control algorithm, the fuzzy PID control algorithm has the advantages of small overshoot, high control precision and strong anti-interference ability. The simulation test in Simulink environment shows that the overshoot of the system is reduced under the algorithm σ, which can be controlled within 1% and the adjusting time t is controlled within 0.5s, which can realize the stable control of the yaw angle, pitch angle and roll angle of the stabilized platform.


2010 ◽  
Vol 24 (8) ◽  
pp. 786-790
Author(s):  
Qingli Ou ◽  
Xingzhong Wu ◽  
Li Cui
Keyword(s):  

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