FIELD: unmanned aerial vehicles.
SUBSTANCE: invention relates to a method for controlling the thrust of a vertical takeoff and landing unmanned aerial vehicle with cyclic propellers. To control the thrust, the blades are rotated, rotating around their own axis, as well as rotating around the axis of the propeller driven by electric motors. The angle of installation of the propeller blades is controlled electronically by means of an on-board computer of an unmanned aerial vehicle, which processes the signals of the angular position sensors, using electromechanical actuators, with which each blade is equipped.
EFFECT: invention provides optimal settings for the positions of the blades for each propeller, reducing drag on the propulsion elements by reducing the number of mechanically loaded elements.
1 cl, 3 dwg
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