FIELD: aircraft lateral movement control systems. SUBSTANCE: yawing damper is provided with yawing and rolling angular-rate sensors, summing amplifier, rudder actuator; damper is also provided with aircraft pedal angle sensor, coordinate converter, damper parameter tuning unit, aperiodic filter included between rolling angular-rate sensor and summing amplifier. EFFECT: extended range of lateral movement; improved quality of transient processes during flight of aircraft in wide range of change of angle of attack; improved aerodynamic characteristics. 6 dwg
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