Abstract:Aiming at the problem that the system designed with nonlinear ADRC technology and the system designed with linear ADRC technology are affected by noise, which leads to the obstruction of signal transmission and the low accuracy of yaw Angle tracking control results, a design of uav yaw Angle tracking control system based on nuclear correlation filtering was proposed. Under the support of the overall system architecture, STM32F407 master control chip is adopted to ensure the stability of uav control system. Steering Angle sensors are mounted under the steering wheel to provide the steering wheel for the ESP electronic control unit. The 2.4ghz remote control receiver is used to generate PWM signals with different pulse width.By controlling the rotor yaw controller, the rotor is pushed to rotate under instructions from different angles. The target image is filtered by the nuclear correlation filter, the target motion position is estimated by the transport of the filter, and the ground reference coordinate system and the frame coordinate system of the UAV are determined, which constitute six degrees of freedom of the UAV in the space. Thus, the yaw Angle tracking and control software flow is designed to track and control the yaw Angle of the UAV. The experimental results show that the roll Angle of the system is consistent with the actual value trajectory, and the error is 0. There is a deviation between the pitch Angle and the actual value trajectory with an error of 0.05°, which provides system support for the uav to fly accurately in different directions.