Research on FCS Design Technology of Electric Tilting Quadrotor UAV.

Tilting quadrotor aircraft not only has the advantages of tilting twin-rotor aircraft, such as vertical takeoff and landing, free hovering and long-range transportation, and high-speed cruise, but also can improve the flight performance, carrying capacity and maneuverability of the aircraft. Taking a 100kg electric tilting quadrotor UAV as the target platform, the design technology of flight control system of the UAV was studied, including the reasonable and feasible system configuration, software and hardware development technology, system control law design technology, and the establishment technology of simulation platform of the system. The results show that the technical approach for the design of the flight control system of the electric tilting quadrotor is effective and can satisfy the operation requirements of the UAV.