Modern state, problems and trends are discussed for mini Unmanned Aerial Vehicles (mini-UAV) with reference to development of advanced mini-UAV relating to various missions. Some major concepts are considered for these UAV especially in view of their mission goals, motion and mission control schemes, typical structural features for mini-UAV together with corresponding ground service and control tools. Advantages and disadvantages are analyzed for several mini-UAV motion and mission control schemes. Some data are listed about financing for a number of programs associated with UAV research and development. Features are derived and discussed for a new class of UAV namely micro-UAV.
Problems associated with a motion simulation for vehicles moving through resisting media are considered with special emphasis to mini Unmanned Aerial Vehicles (mini-UAV). Areas of theoretical and experimental investigations are discussed with reference to modern understanding for such processes as well as measuring system capabilities. An experimental approach is suggested to simulate quasi-free controlled motion of the vehicles. This approach is based on wind tunnel experiment by using mounting with multiple degrees of freedom.
In the paper are presented the considerations on the possibilities of using In micro unmanned serial vehicle (MUAV) of new materials construction. The authors reveal the interdependence of the components of the PAN carbon composite and nanocomposite in the statistical aspects by studying the physical and mechanical properties of the components.
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