FIELD: unmanned gliding aircrafts.
SUBSTANCE: invention relates to a method for correcting the formed configuration of the route of an unmanned gliding aircraft (UAV). To correct the formed route configuration, the route is set by reference points in the form of a set of geodetic coordinates, the values of the rotation angles are determined at the reference points, and if, when compared with the permissible values of the angles set in advance and specified in the table in the function of the flight range, a difference is found that causes a violation of the specified technical restrictions on the controllers parameters of the UAV, then, according to the rules of spherical trigonometry, the problematic reference point is iteratively shifted to small distances with a decrease in the rotation angle value of the route to an acceptable one. EFFECT: correction of the formed UAV route is provided in case of non-fulfillment of technical restrictions at reference points.
1 cl, 2 dwg, 1 tbl
