FIELD: control systems of homing missiles, in which occurs interrupted transmission of information to the input of the homing head.
SUBSTANCE: the antenna of the homing head is turned to the target after disappearance of the signal reflected from the target at an alternating rate proportional to the current evaluation of the angular error formed by integration of the difference of the angular rate of the sight line obtained from the optimum detecting filter used for formation of control commands in the homing system, and its value measured by the homing head. The zero value may be also used as an estimate of the angular rate.
EFFECT: enhanced accuracy of homing.
2 cl, 4 dwg
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