Design and Simulation of Autonomous Landing Control System for Unmanned Aerial Vehicle Based on Dynamic Inversion
Based on the research background of how a carrier-borne unmanned aerial vehicle(UAV)lands on an aircraft carrier according to a predetermined landing trajectory,a control tracking method based on dynamic inversion design is proposed.A nonlinear 6-degree-of-freedom model of the UAV is established.Interference from the wake of the ship and the movement of the aircraft carrier is added to the landing process.A dynamic inverse controller is designed to control the landing.The simulation results show good landing performance with a 98％success rate.
dynamic inversioncarrier air wakelanding controlcarrier-borne unmanned aerial vehicle
万方数据
维普
