STUDY OF FLIGHT-TECHNICAL PARAMETERS OF CONVERTOPLAN-TYPE UNMANNED MICRO AIRCRAFT IN MULTICOPTER MODE

Abstract

In the article, the on-board measurement-recording system designed to record the main flight parameters of the convertoplan-type micro-unmanned aerial vehicle and the base of elements that make up the system are described. In the test flights performed in multicopter mode at different times and in meteorological conditions, both the temperature, current consumption and number of cycles of each of the motors, as well as the angle change and acceleration of the glider along the three coordinate axes were measured and recorded by means of the on-board measuring and recording system. Graphs of the time dependence of the recorded parameters were constructed, and based on them, the take-off, landing and hovering modes of the aircraft were studied. The possibility of diagnostic testing of power elements on the ground during preparation for flight, control of flight events that may occur in the air during flight is shown.