Autonomous control of running takeoff and landing for a fixed-wing unmanned aerial vehicle

摘要

This paper concerns about automatic flight control strategies for the running takeoff and landing of fixed-wing unmanned aerial vehicles (UAVs). Firstly, a dynamic model of fixed-wing UAVs is developed. Then the takeoff and landing control strategies are designed. The flight control strategies are designed to be segmented. A fixed-wing UAV named "Petrel" is used as an experimental platform. Finally, the flight experimental results are proposed to validate the automatic running takeoff and landing controller.