FIELD: aviation equipment. SUBSTANCE: for increase of accuracy of guidance sensitivity axis of directional vehicle-born aerial is positioned at angle 35-50 deg to symmetry plane of gliding parachute. Gliding of parachute is controlled so that flight about cone of radio silence of radio beacon is realized. Use of invention makes it possible to perform automatic landing of gliding parachute systems under conditions of wind disturbances with sufficient accuracy. EFFECT: increased accuracy of guidance. 2 cl, 2 dwg
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