The invention discloses an oil and
electricity hybrid multi-rotor unmanned aerial
vehicle control system and method. The oil and
electricity hybrid multi-rotor unmanned aerial
vehicle control system comprises a
fuselage and a plurality of rotors evenly arranged on the side faces of the
fuselage at intervals. An engine module, a generator module and a cradle head
assembly are arranged at the bottomof the
fuselage, and an
oil tank is arranged at the top end of the fuselage. A
control system body is arranged in the fuselage, and the fuselage comprises a first fixing board and a second fixing board. The engine module, the generator module and the cradle head
assembly are arranged at the lower end of the first fixing board, and the engine module is connected with a generator and can drive thegenerator to operate. The generator and the cradle head
assembly are electrically connected with the
control system body. The
control system body comprises a plurality of control main boards arrangedbetween the first fixing board and the second fixing board, the control main boards comprise power supply main boards, and an image transmission main board, an engine and
generator control main board,a flight control main board, a
remote control main board and a plurality of control interfaces are formed in the power supply main boards, wherein the image transmission main board, the engine and
generator control main board, the flight control main board, the
remote control main board and the multiple control interfaces are formed parallel to the planes where the power supply main boards are located.