FIELD: weapons and ammunition.
SUBSTANCE: invention relates to military equipment, and namely to guidance systems of controlled missiles. For that purpose, a system includes a control drive, a sight, a controlled missile, a launching unit, a command line, a coordinator, a control signal generation unit, an adder, a control command generation unit, a switch, a controlled missile trajectory stabilisation unit, an air flow velocity sensor, a quad unit, a scaling unit, an inverter, an air flow angular position sensor that consists of n sensitive elements of photo receivers, a unit for determining the direction of air flow movement, and a unit for determining a sign of direction of the air flow movement. The unit for determining the direction of the air flow movement includes n NOT elements, n decoders and an OR element.
EFFECT: higher accuracy.
2 cl, 6 dwg
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Authors
Dates
2015-01-27—Published
2013-11-06—Filed