FIELD: missiles, in particular, topographic referencing and targeting of missiles using satellite signals. SUBSTANCE: method involves detection of coordinates of missile launch point by means of processing of information received from radio navigation channels of satellite navigation system and solving time-navigation problem in order to achieve angular orientation of missile in space using calculation of target angle and its constituents. EFFECT: increased functional capabilities for detection of position coordinates, increased speed for preparing and launching high-accuracy missiles. 2 dwg
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