FIELD: aviation.
SUBSTANCE: invention relates to aircraft control systems, made according to “regressive weathercock duck” diagram. System of front horizontal “duck” fins control comprises a rudder indexing mechanism, a rudder position sensor, a sensor of vertical sliding an amplifier with three inputs, a rudders' actuator, connected in a certain manner.
EFFECT: higher reliability and simpler design of aircraft.
3 cl, 3 dwg
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