FIELD: development of missile guidance systems.
SUBSTANCE: three-position reference periodic missile rolling modulating signals are normalized that are shafted relative to one another by angle π/2. The relay control signals are multiplied by three-position reference periodic missile rolling modulating signals corresponding to them. The device has a gyroscopic sensor of modulating signals containing a commutator consisting of four conducting sector insulated from one another.
EFFECT: enhanced accuracy of guidance of rolling missiles with relay drives of control members.
5 dwg
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