Hybrid gasoline and electric power aircraft balance control system

The invention discloses a hybrid gasoline and electric power aircraft balance control system. The system comprises a data processing center, a sensing center, a first control unit, a second control unit, a gasoline engine, motors and a wireless transmission module, wherein the sensing center comprises a first power sensor, multiple second power sensors and multiple state sensors, the quantity of the motors is four or an even number greater than four, the motors and the second power sensors are identical in quantity, the first power sensor is used for monitoring engine power of the gasoline engine, the second power sensors are used for monitoring rotation speeds of the motors, the state sensors are used for acquiring attitude data, the gasoline engine is used for providing lifting force in a vertical direction, and the motors are used for providing movement force and flight balance force. The system is advantaged in that the structure is novel, the gasoline engine and the motors realize clear work division, wo