FIELD: aircrafts.
SUBSTANCE: invention relates to a method for including a preformed maneuver into a flight mission of an unmanned gliding aircraft (UAV). To include the maneuver in the flight task, the conditional coordinates of the control points of the maneuver are transformed in a certain way. The obtained coordinates of the control points are included in the data of the flight mission of the UAV. To a given set of reference points of any maneuver in the conventional coordinate system, one more reference point is added in advance in the vertical coordinate plane at a distance from the point considered to be the first, sufficient to turn the UAV with maximum speed in the direction of the second reference point of the maneuver. The last reference point of the UAV trajectory sustainer is set at a distance from the target equal to the distance of the first UAV maneuver point from the origin of the conventional coordinate system.
EFFECT: improved UAV guidance accuracy.
1 cl, 3 dwg, 2 tbl
