UNMANNED AERIAL VEHICLE CONTROL METHOD AND FLIGHT CONTROL ACTUATING UNIT FOR METHOD ACTUALIZATION Russian patent published in 2017 - IPC B64C13/00 F03D3/00 

FIELD: aviation.

SUBSTANCE: method is carried out by the velocity vector direction regulation by means of the change of the frontal resistance to the approach flow and of the thrust vector value of the blowdown jet due to the change of the approach flow velocity energy within the airfoils, in accordance with the guidance command. The flight control actuating unit arrangement comprises the body with the rigidly fixed airfoils with the air inlet and air bleeding ducts. There are flight control actuator and accumulator battery within every airfoil. The flight control actuator is comprised of the actuating unit of the steering engines that are designed as the coaxially situated electric motor and turbine. The electric motor is the commutatorless one with the outer rotor, on which the turbine is mounted. The floating battery is used in the function of the accumulator battery.

EFFECT: enhancement of the functional possibility of the unmanned aerial vehicle application on the slow speed and high altitude, manufacturing simplification.

4 cl, 6 dwg