FIELD: aircraft engineering.
SUBSTANCE: proposed device comprises control signal digital master, comparator, first amplifier, angle digital transducer, angular speed transducer, second amplifier, first adder, ADC, digital differentiator, third amplifier, second adder, first, second and third constant signal generators, ram pressure metre, first, second and third dividers.
EFFECT: expanded operating performances, higher accuracy of control.
2 cl, 1 dwg
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