FIELD: instrument engineering, applicable in on-board systems of automatic control of flight vehicles.
SUBSTANCE: the control unit has a control signal selector, pitch-angle pick-off, pitch-rate pick-up, integrator, summing amplifier, reference signal selector, first and second multiplier units, functional signal limiter, flying-velocity transducer, division unit and a ram air-pressure sensor.
EFFECT: expanded functional capabilities.
1 dwg
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