CONTROLLED MISSILE GUIDANCE SYSTEM Russian patent published in 2015 - IPC F41G9/00 

FIELD: weapon and ammunition.

SUBSTANCE: system has a control drive, a sight, a controlled missile, a launcher, command transmission line, a coordinator, a control signal generation unit, an adder, a control commend generation unit, a key, controlled missile trajectory stabilisation unit, air flow speed sensor, a squarer, a scaling unit, an inverter, an air flow angular speed sensor which consists of n-sensitive elements of photodetectors, air flow movement angular speed determination unit which contains n-first elements and n-second NOT elements, n-decoders, the first, second and third OR elements, n-threshold devices, a set unit, a differentiating circuit, a shift register, a signal generator, n-elements AND, n-counters.

EFFECT: improvement of efficiency of firing by controlled missiles.

3 dwg