FIELD: weapons.
SUBSTANCE: invention relates to rotating missile control systems. Proposed converter comprises demodulator connected to inputs of converter that converts the signals of reference and signal coils incorporated with angle transducer, and low-frequency filter with its input connected to demodulator output and output making converter first input. Proposed converter comprises additionally pulse generator and pulse counter with its data input connected to output of master oscillator. Pulse output connected is connected to S-inputs of first and second triggers. First trigger output is connected to second trigger D-input, second trigger C-input being connected to pulse generator output, first trigger R-input and counter R-input. Second trigger output is connected to control input of the gate connecting supply voltage to converter second output designed to feed angle transducer motor. Master oscillator output is connected to pulse generator second input, pulse generator first input being connected to converter that converts the signals of reference and signal coils incorporated with angle transducer.
EFFECT: higher accuracy, reduced mode-change time interval.
3 cl, 2 dwg
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Authors
Dates
2010-02-20—Published
2005-06-07—Filed