Keyword: «unmanned aerial vehicle (uav)»
The article considers the results of mathematical modeling of the flywheel motion of a single rotor blade, obtaining integral characteristics of a single rotor, calculation features of the carrier system with coaxial propellers, modeling the approach of helicopter blades of a coaxial scheme.
The article discusses the possibilities of various types of weapons of destruction, from the helicopter armament complex, from the point of view of the expediency of their use in solving the problem of countering unmanned aerial vehicles. Options for improving these systems and ways to increase the effi-ciency of their use are proposed.