Analysis of Exchange Power in the Power System of Drone

The classification of drones - both military and civilian according to the relevant criteria is presented. Block diagrams a typical unmanned aerial vehicle its power system are shown. Typically, drone "micro", "mini" or "short range" category, UVS international classification, set DC / converters with microprocessor control system. source for such aircraft usually battery, less often fuel cells. During flight, engine speed variable, change depends not only on changes in flight direction, but also weather conditions, as wind, stabilization constantly aligns drone. This leads fact that supply device actually significant part time transition condition. content component exchange energy battery consumed which turn will increase losses, thus reduces range vehicle. phenomenon occurrence systems electric vehicles powered from sources specifically an analyzed. current, voltage, active inactive components mains network locomotive DE1 illustrated. It can be seen sharp modes operation traction units there motor-network Such processes almost any associated presence number reactive elements systems, well frequent load parameters. A block diagram consists three parts: air part, itself, ground station, autonomous manned, system, provides communication data transmission. presented simplified schematic motor relations determining amount derived. concluded reduce impact this phenomenon, it necessary modify by adding compensation component.