A hybrid control method based on backstepping and fuzzy adaptive Proportion-Integration-Differentiation (PID) was proposed, which improved the flight stability of quadrotor aircraft in different environment. The method selected the current appropriate controller according to the Unmanned Aerial Vehicles (UAV) flight environment, large attitude angle, and large attitude angular velocity. In the case of the system undisturbed, backstepping-based control algorithm could complete trajectory tracking. In case of disturbance, fuzzy adaptive PID could greatly suppress the impact of disturbance and realize the precise control of quadrotor aircraft. The Matlab simulation analysis and practical experiments illustrate that the stability augmentation hybrid controller can effectively realize the stability.