The utility model discloses a three-axis tilt rotor vertical take-off and landing aircraft, and belongs to the technical field of
aviation. A side canard type triangular distribution structure is adopted, the flight
gravity center is arranged in a connecting line of three propellers, and the vertical lifting stability is remarkably enhanced. The unmanned aerial vehicle is provided with a unique rotor wing
system, a horizontal wing
system and a switching mechanism, and efficient switching between vertical flight and horizontal flight can be achieved. During flight, the rotors vertically provide lift force in the take-off stage, the inclination angles and the
pitch angles of the rotors are adjusted in the conversion stage, and the horizontal wings bear main lift force during horizontal flight. A flexible
engine management strategy, an efficient
fixed wing take-off mode and the like are further arranged. In mountainous area rescue,
urban logistics and other implementation cases, the unmanned aerial vehicle has the advantages of flexible take-off and landing, efficient flight, accurate control and the like. The aircraft can save
energy consumption by 20%-40%, the
takeoff taxiing distance is shortened by 30%-60%, the
flight speed is increased by 15%-30%, the voyage is increased by 20%-35%, and the aircraft can be widely applied to multiple fields such as
emergency rescue and cargo transportation.