FIELD: military engineering.
SUBSTANCE: method involves following and measuring target coordinates using thermovision system relative to thermovision raster, launching rocket missile and reckoning current time from the moment of its start, capturing, guiding and measuring rocket coordinates with infrared location finder, processing rocket deviation from target with axial rocket coordinates mismatch between coordinate values measured with thermovision system and infrared location finder system.
EFFECT: enhanced effectiveness and high accuracy of guidance.
3 cl, 1 dwg
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