ON-BOARD CONTROL AND MEASURING COMPLEX FOR SMALL-SIZED СONVERTIPLANE UNMANNED AERIAL VEHICLES TYPE

Abstract

The article describes an on-board control and measuring system designed to record the main flight parameters of a small-sized (mini) сonvertiplane type unmanned aerial vehicle and the element base used for this. The scientific literature published in this direction and the results of tests carried out in a stationary mode through an on-board control and measurement system are analyzed. Using the on-board control and measuring system, a diagnostic check and assessment of the engine condition were carried out. Ground-based diagnostics of the power elements of a small-sized (mini) unmanned aerial vehicle before and after flight are shown, as well as the ability to control flight events that can occur in the air during flight