GUIDANCE SYSTEM OF CONTROLLED MISSILES Russian patent published in 2011 - IPC F41G9/00 

FIELD: weapons and ammunition.

SUBSTANCE: proposed device includes adder connected between generation unit of control signals and generation unit of control commands, in-series connected switch the input of which is connected to the second output of coordinator, air flow velocity sensor kinematically connected to start-up unit, squaring device, scaling unit and inverter the output of which is connected to the second input of adder, as well as stabilisation unit of trajectory of controlled missile, the input of which is connected to the third output of coordinator, and output is connected to the third input of adder.

EFFECT: increasing the probability of hitting during firing in the described conditions by using the proposed guidance system.

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