METHOD OF REDUCING THE SPEED AND TIME LOSS IN IMPLEMENTATION OF MANEUVRE OF SPECIFIED CONFIGURATION BY UNMANNED AERIAL VEHICLE OF VOLPLANE TYPE

摘要

FIELD: aviation.;SUBSTANCE: to implement the maneuver, the initial boundary guidance problem is divided into a set of intermediate boundary problems, in which the required values of the control parameters for the aerodynamic bank and the angle of attack, calculated for each reference point in each guidance cycle, are small throughout the guidance time, and stick force on the aerodynamic controls of an unmanned aerial vehicle is formed.;EFFECT: reducing of speed and time of motion loss of unmanned aerial vehicle.;3 dwg, 2 tbl