FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises pitch angle master, pitch angle robot pilot computer, algebraic selector, elevator servo drive, pitch angle transducer, master of the maximum angle of attack, computer of automatic limiter of the angle of attack, transducer of the angle of attack, master of maximum normal overload, computer of maximum normal overload automatic limiter, normal overload sensor.
EFFECT: accurate limitation of limiting aircraft parameters, smooth transient processes at switching of control channels.
2 dwg
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