FIELD: physics, navigation.
SUBSTANCE: invention can be used for radar identification of aircraft on all possible ranges and aspect angles of a location. Said technical result is achieved due to that identification of an aerial object takes into account not only match of the relative positions of scattering centres of the surface of the aerial object along the line of vision, but amplitude thereof, which provides better identification characteristics.
EFFECT: more accurate automatic identification of aerial objects in the quasi-optical region of reflection of radio waves by establishing stricter congruence between real and reference range portraits, and specifically owing to additional information on amplitude of pulse responses in the structure of the range portrait.
1 dwg
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