The invention relates to a vertical take-off and landing aircraft, belonging to the technical field of aircraft, comprising a fuselage, a wing, a reversing lifting device, a vertical lifting device, asteering propeller and a sled landing gear. A main control is arranged in that fuselage, and the main control is connected with a reversing lifting device, a vertical lifting device and a steering propeller. The wing is swept back. The reversing lifting device is located at the trailing edge of the wing and can be steered 90 degrees under the control of the master controller to provide vertical lift or forward thrust for the aircraft. The vertical lifting device provides upward lifting force for the aircraft in the form of rotating blades driven by an electric motor, and the vertical liftingdevice is arranged at the front end of the fuselage. The steering propeller is located below the vertical lift. The invention can be used for vertical take-off and landing, long sailing time, stable flight process and high safety factor, and is suitable for logistics transportation, air fire extinguishing, post-disaster rescue and the like.