GUIDANCE SYSTEM OF GUIDED MISSILES Russian patent published in 2015 - IPC F41G9/00 

FIELD: weapons and ammunition.

SUBSTANCE: system comprises a control drive, a launcher, a sight, a coordinator of the guided missile, a unit of generating control signals, a unit of generating of output control commands, the command transfer line, control equipment of the guided missile, an adder, a key, a speed sensor of the airflow, a quadrator, a scaling block and an inverter, a unit of trajectory stabilisation of the guided missile, an angular position sensor and a unit of determining the angular position of the air flow. The unit of determining the angular position of the air flow comprises a plurality of logic elements.

EFFECT: increase in efficiency of firing the guided missiles.

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