FIELD: aircraft engineering.
SUBSTANCE: system of control at ground run by rudder and nose wheel comprises control member connected with rudder actuators and nose wheel actuators that can deflect to the right and left from neutral position. Every deflection of control member from neutral position at aircraft every speed complies with rudder and node wheel deflections defined unambiguously. Note here that said neutral positions of said control member and nose wheel are those the latter stay at when control member and nose wheel actuator are communicated as required.
EFFECT: safe ground run at manual and automatic control and side wind.
4 cl, 8 dwg
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