UAV Flight Control System Design Based on Ardupilot

Aiming at the flight control system of the compound UAV, this paper introduces each module of the control system, including the main control chip, altimeter, inertial navigation system, altimeter, magnetometer, etc., studies the dynamic model of the UAV, and re-designs and develops the flight control source code architecture of the compound UAV in terms of software code. Finally, the flight path planning is carried out in the ground station, and it can be seen that the aircraft smoothly flies along the predesigned route, which proves the effectiveness of the UAV flight control system designed in the paper.