The application relates to the technical field of
automatic control of unmanned aerial vehicles, in particular to a
control system of an unmanned aerial vehicle, which comprises a
bus, a self-
pilot, a plurality of
rudder controllers and a plurality of
rudder surface driving mechanisms, the self-
pilot and each
rudder controller are connected to the
bus, each rudder controller is electrically connected with the corresponding rudder surface driving mechanism; each rudder controller is provided with a control distribution table mapped with a flight configuration; during the flight of the unmanned aerial vehicle, each rudder controller determines the corresponding control distribution table according to the flight configuration broadcast by the self-
pilot; according to the control distribution table, the weight of each
control signal participating in control is determined, and the total
control signal is obtained by weighted summation of each
control signal participating in control; each rudder controller outputs the total control
signal to the corresponding rudder surface driving mechanism to realize the control of the rudder surface driving mechanism. That is, the application scheme can relieve the operation and storage pressure of the self-pilot, simplify the configuration of the self-pilot and improve the universality of the self-pilot.