FIELD: unmanned aerial vehicles.
SUBSTANCE: method of launching unmanned aerial vehicle (1) consists in the fact that orientation of tubular launcher (2) is performed in azimuthal and elevation planes. In onboard equipment of UAV there performed is input of flight task, including time of UAV reaching the top of ballistic flight trajectory. Wherein a cased propellant charge is installed in the channel of the tubular launcher behind the UAV, obturation, acceleration and removal of UAV (1) from tubular launcher (2) under the influence of the total thrust of the propellant charge gases. At the moment of time corresponding to the top of the ballistic flight trajectory, the UAV cruise engines are launched.
EFFECT: high efficiency and accuracy of guidance.
4 cl, 6 dwg, 2 tbl
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