Abstract:
Addressing the flight trajectory tracking and attitude control of four-rotor unmanned aerial vehicles(UAVs),this study presents a comprehensive dynamic model for quadrotors.A controller based on a nonlinear model predictive control algorithm is designed specifically for this dynamic model, facilitating trajectory tracking and attitude control of the quadrotor UAV with constraints on input and output states, as well as notable anti-interference capabilities.The feasibility of the proposed method is verified by numerical simulation experiments.