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

FIELD: weapons and ammunition.

SUBSTANCE: guidance system of guided missiles comprises a control drive, a sight, a guided missile, a launcher, a command transfer line, a coordinator, a unit of generating control signals, an adder, a unit of generating of control commands, a key, a unit of trajectory stabilisation of the guided missile, a speed sensor of the airflow, a quadrator, a scaling block, an inverter, an angular position sensor, a unit determining the direction of air flow, a the unit determining the direction of air flow comprises n NOT-gates, n-decoders, OR-gate, a memory block, a subtracting unit, the first and second diodes.

EFFECT: increased efficiency of firing the guided missiles.

3 dwg