Aircraft dual channel coordinated controller

FIELD: transport. SUBSTANCE: invention relates to aircraft ACS onboard systems control devices with implementation of coordinated turn modes. Control device configured in compliance with this invention allows functional variation of control intensity at variation of governing effects in the wide range. Control device comprises roll angle transducer, roll angular velocity transducer, heading angle transducer, heading angular velocity transducer, heading control signal generator, first and second subtractors, inverting amplifier, first and second nonlinear elements with constriction, nonlinear element with insensitivity zone, amplifier and signal limiter. EFFECT: higher static and dynamic precision of control. 1 dwg