FIELD: weapons and ammunition.
SUBSTANCE: in flight the speed vector of the missile is controlled so that it was aimed at the target along the line of the direction vector "missile-target", the sides of deviation of the speed of motion of the missile is determined relative to the direction of the speed vector "missile-target" based on decomposition of the total speed of "missile-target" into two components: radial and tangential, and simultaneous evaluation of radial and tangential component of the total speed "missile-target". At that the relative values of the Doppler frequencies of radial and tangential component may be either equal with each other or relatively larger or relatively smaller, at that, respectively, the stress ratios Zi will change, formed by these speeds.
EFFECT: improvement of guidance accuracy.
2 cl, 3 dwg
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