A method for determining a target steering angle for nose landing gear of an aircraft includes receiving rudder pedal input data into a steering control unit, receiving aircraft speed data into the steering control unit, calculating a normal gain, calculating a parking gain, and adding the normal gain and the parking gain to determine the target steering angle. The normal gain is a positive quantity in all aircraft speed and pedal stroke ranges. The parking gain is a positive quantity in parking and taxiing speed ranges. A nose wheel steering system is also disclosed.


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    Title :

    VARIABLE GAIN CONTROL NOSE WHEEL STEERING SYSTEM


    Additional title:

    LENKSYSTEM FÜR EIN BUGRAD MIT VARIABLER VERSTÄRKUNGSSTEUERUNG
    SYSTÈME DE DIRECTION DE ROULETTE DE NEZ PAR COMMANDE À GAIN VARIABLE


    Contributors:

    Publication date :

    2017-05-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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