A four rotor UAV flight control system is designed. First, the dynamic system model of the four rotor UAV is established, including the Kinematics equation, dynamic equation, and system control distribution model. Then, based on the dynamic system model, a double closed loop control system is designed, in which the attitude loop is the inner loop of the control system, and the position control loop is the outer loop of the control system. Finally, MATLAB software is used for experimental simulation verification, Set up two operating conditions: wind interference and unmanned interference, then compare and analyze the simulation results. The experimental results show this four rotor unmanned aerial vehicle flight control system has strong anti-interference ability and meets the requirements of engineering design standards specially.
Design and Simulation of Flight Control System for Quadrotor UAV
2023-05-19
1388102 byte
Conference paper
Electronic Resource
English
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