FIELD: aviation.
SUBSTANCE: invention relates to unmanned aerial vehicles (UAVs). Method of placing the UAV in the high-altitude flight trajectory includes placing and fixing the UAV on the launch pad of the aircraft carrier along the fuselage, flight of the aircraft carrier to the height of the separation of the UAV, its separation, stabilization of its position by the control system, launch of the booster engine and control in autonomous flight with an increase in the pitch angle. UAV is provided with pulsed jet engines to create a rotational pulse around a transverse axis passing through the center of gravity of the UAV and compensate for this rotational impulse. Increasing the pitch angle is performed before starting the booster engine by turning on a jet engine generating a rotational pulse. In the process of increasing the pitch angle to the required value, the jet engine of rotational pulse compensation is turned on, and the start of the booster engine is ensured after reducing the angular velocity of the UAV rotation around the transverse axis.
EFFECT: technical result of the invention is to increase the safety of the launch of the UAV on the high-altitude flight path.
1 cl, 2 dwg
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Authors
Dates
2019-03-22—Published
2018-03-16—Filed