FIELD: navigation systems.
SUBSTANCE: invention relates to a method of directing an aircraft to a single radiation source. Method comprises determining a heading angle during direction-finding on a radiation source, aligning a straight line of a predetermined path through a direction finding point towards a source, withdrawing aircraft on line of preset path, and if heading angle exceeds preset one, aircraft is rotated along circumference with minimum possible radius to opposite side from source of single radiation and aircraft is brought to line of preset path with zero path to source of radiation along shortest route.
EFFECT: higher probability of guidance of aircraft on source of single radiation.
1 cl, 3 dwg
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