The invention relates to a hybrid power unmanned aerial vehicle. The hybrid power unmanned aerial vehicle is characterized by comprising at least two lifting rotors, control rotors, a load frame and a rack, wherein the lifting rotors, the control rotors and the load frame are all mounted on the rack; the lifting rotors are symmetrically arranged in pairs and are arranged on two sides of the central axis of the unmanned aerial vehicle, and the rotor faces of the lifting rotors are perpendicular to the central axis of the unmanned aerial vehicle; and the lifting rotors are driven by fuel motors, and the control rotors are driven by motors. According to the hybrid power unmanned aerial vehicle, the lifting rotors provide the main lifting force; the control rotors keep the attitude of an aircraft; during advancement, retreatment and selective movement in a plane, the control rotors are accelerated or decelerated to change the attitude of the aircraft; the control algorithm of the unmanned aerial vehicle is similar to that of the multiple rotors, and a matched control structure of a helicopter is omitted, so that the structure and the control algorithm are greatly simplified, and further, the stability, the load, the flight duration and the controllability of the aircraft are improved.