PRELIMINARY DESIGN OF A CLOOSED LOOP SYSTEM STABILIZING STATE VARIABLES OF THE LATERAL MOTIONN OF AN UNMANNED AERIAL VEHICLE

In the article are shown results of the analysis made on the flight-mechanical mathematical models of the unmanned aerial vehicle (UAV) “Szojka-III”. Analysis was done on the vehicle flying on a state level (400 m) with a state mass (m=135 kg) and at different speeds (110, 130, 150,170, 190km/h).