ESTIMATION OF THE OPERATION STABILITY OF THE MECHATRONIC RIVER UNIT OF A UAV WITH A DIGITAL CONTROL SYSTEM
The paper presents the results of a mathematical analysis of the stability assessment of the mechatronic unit of the prototype of the UAV adaptive wing model. Emphasis is placed on the stability of technological and operational characteristics, which is not detected in the process of virtual simulation. The question of the possibility of going beyond the permissible limits of an adjustable parameter in spite of the mathematical probability of the expected result of the task execution is presented for discussion.