Analytical Synthesis of Control Acceleration of Unmanned Aerial Vehicle

. The problem of analytical synthesis the control acceleration for an unmanned aerial vehicle (UAV) during its flight along a complex trajectory, consisting sequentially located horizontal sections, at different heights relative to earth's surface has been solved in paper. as definition optimal linear non-stationary system specified minimized quality functional. mathematical model is presented form differential equations UAV motion vertical plane fixed coordinate related surface. A feature proposed methodology solving substantiation original functional and parameters included law variation obtained by known methods. As components functional, values coordinates velocity are considered they corresponding points space through which path must pass, order obtain curvature trajectory. derived dependences make it possible implement them on board aircraft and, ultimately, solve ensuring minimum energy consumption when controlling object (UAV). Computer simulation analytically results trajectory processes changing speed have shown efficiency technique prospects use initial stage system.