FIELD: aircraft engineering.
SUBSTANCE: proposed device comprises angle selector, three comparators, two multipliers, three adders, angle, angular speed and speed head transducers, divider, three reference signal selectors, controlled switch, six scale amplifiers, three D/A converters, AND logical element, controlled switch, differentiating link, negative polarity isolation unit, anti-flexure signal.
EFFECT: higher accuracy of control.
1 dwg
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