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 control commands, an adder, a key, a speed sensor of the airflow, a quadrator, a scaling block, an inverter, a unit of trajectory stabilisation of the guided missile, a correction unit, the correction unit comprises n threshold devices, a signal setup unit, a differentiating circuit, the first and second OR elements, a shift register, a signal generator, n and-gates, n NOT-gates, n counters.

EFFECT: increase in efficiency of firing the guided missiles.

2 dwg