Tilting body type hybrid multi-state aircraft with operating control surface

The utility model provides a tilting body type hybrid multi-state aircraft with an operating control surface. The aircraft comprises a body, wherein the body comprises two fixed wings which are symmetrically arranged in parallel and a middle support frame; four sets of rotors are arranged on the two fixed wings; the operating control surface is arranged on the two fixed wings; and rotation of the control surface is controlled by virtue of a steering engine, and the actions of pitching, rolling and adjusting the course angle are realized. The advantages of a multi-rotor aircraft and a fixed wing aircraft are integrated, and multiple rotors and operating control surface are arranged on the multiple fixed wings. In all the parts, the rotating shafts of the propeller and the motor, the steering engine, the steering engine operating lever and the control surface can normally rotate, and the relative positions of the other components do not change. Particularly, the mounting positions of the body, the motor and the propeller are relatively fixed, and totally three flights are formed, namely a vertical take-off and landing or spot hover state, a cruising flight state and a transition state.