An aircraft landing gear longitudinal force control system (20) for an aircraft having landing gears with braking and/or driving wheel(s). The system includes an error- based force controller (21) having feedback for minimising any error between the demanded force (Fx*) and the actual force (Fx_LG) achieved by the force control system. The feedback may be derived from force sensors on the landing gear for direct measurement of the landing gear longitudinal force. The force control system may include an aircraft level landing gear total force controller and/or a landing gear level force controller for each actuated landing gear.


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    Titel :

    Aircraft landing gear longitudinal force control


    Beteiligte:

    Erscheinungsdatum :

    2015-09-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60T Bremsanlagen für Fahrzeuge oder Teile davon , VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF



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