The application discloses a novel multi-
mode control transverse double-rotor unmanned helicopter, which comprises an unmanned aerial vehicle shell, a
differential transmission module, a lift balance module, a pitching control module and a
remote control system, wherein the
differential transmission module comprises a brushless
drive motor, a rotating shaft fixed wheel, a mechanical differential device, an electromagnetic speed control device and a rotor rotating shaft; the lift balance module is used for realizing the
angle of attack change of the self-rotating rotor of the unmanned aerial vehicle; the pitching control module is used for realizing the rapid adjustment of the pitching attitude of the unmanned aerial vehicle; and the
remote control system realizes the multi-
mode control of the unmanned aerial vehicle through
signal transmission. Through the cooperation of the lift balance module, the
differential transmission module, the pitching control module and the
remote control system, the unmanned aerial vehicle can effectively improve the turning maneuvering flexibility, the
flight stability in the full speed range and the pitching attitude response speed, enhance the anti-interference ability and operation reliability in the complex low-altitude environment, and simultaneously simplify the control structure, reduce the overall
power consumption and development and maintenance costs.