Orthogonal design and optimization of flight stability test for the quadrotor unmanned aerial vehicle

The flight stability test of the quadrotor UAV (Unmanned Aerial Vehicle) is an important means to test the correctness of the design scheme of the UAV system. The paper adopts orthogonal design to study the factors that affect the flight stability of the quadrotor UAV. In this paper, several natural factors and control factors, such as wind and throttle control, are taken as the research object. The paper studies the influence of the above factors on the flight stability of the quadrotor UAV, and the algorithm is verified by MATLAB software.