The invention discloses a power
layout and mode conversion control method of a vertical take-off and landing flying wing unmanned aerial vehicle, and belongs to the technical field of
aviation aircrafts. The unmanned aerial vehicle adopts a wing-body fused flying wing type aerodynamic
layout and is provided with four
leading edge power devices capable of independently controlling tilting angles and two rear fixed lift devices, a flight
control system is electrically connected with the power devices, and stable switching of flight
modes is realized through real-time calculation. In the vertical take-off and landing mode, the power device cooperatively provides lift force to realize vertical take-off, hovering and landing; in the
forward flight mode, the power device is adjusted to high-speed
cruise mainly based on the
aerodynamic lift force of the flying wings; and during reverse rotation, the
control system stably swings back the power device and adjusts the thrust, so that safe landing is realized. Efficient and stable conversion between vertical take-off and landing and high-speed
forward flight is achieved, the multi-rotor-wing unmanned aerial vehicle has the multi-rotor-wing flexibility and the fixed-wing high-speed long-
endurance capacity, and the multi-rotor-wing unmanned aerial vehicle is suitable for
urban logistics, area patrol, disaster prevention monitoring, military reconnaissance and other scenes.