FIELD: weapons and ammunition.
SUBSTANCE: invention can be used in guided missiles (GM). The angular velocities of the sight line of target in the vertical and horizontal planes are determined on the signals of projections of the missile velocity and the signals of smoothed coordinates of the missile by summing the signals proportional to the integrals of the projections of the velocity of the signal with the missiles proportional to the smoothed signal differences of the measured coordinates of the missile and the integrals of the measured projections of the missile velocity, the control signals are generated by the rudders proportional to the angular velocity of the sight line of target.
EFFECT: invention enables to provide the necessary accuracy in hitting of GM to the target on signals of the satellite navigation system.
5 dwg
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