FIELD: weapons and ammunition.
SUBSTANCE: guidance system of guided missiles comprises a control drive, a sight, a guided missile, a launcher, a command line, a coordinator, a unit of generating the control signals, an adder, a unit of generating control commands, a key, a unit of trajectory stabilisation of a guided missile, a quadrator, a scaling unit, an inverter, a device of missile ejection, a detection unit of the air flow rate. A detection unit the air flow rate comprises a receiving-transmitting antenna, a switch of transmit-receiving, the first mixer, the intermediate frequency amplifier, the detector, the main oscillator, the power amplifier, the pulse modulator, the second mixer, the intermediate frequency generator.
EFFECT: increased efficiency of guided missile firing.
2 dwg
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Authors
Dates
2015-01-27—Published
2013-11-06—Filed