Design of UAV Flight Control Law Based on PID Control

Abstract

In recent years, UAVs have received more and more attention from countries all over the world. The diverse functions and unique advantages have caused the world to set off an upsurge in UAV development. Taking UAV as the research object, this thesis mainly studies the design of the flight control law of the UAV flight control system based on PID control, so as to facilitate the flight simulation of UAV. In response to this problem, the longitudinal flight control law and the lateral flight control law are designed to maintain and control the movement of the UAV’s altitude, pitching angle, roll angle and course angle.