A flight control law enhances braking efficiency through the operation of aircraft elevators (or another pitch control system) using measured longitudinal acceleration and/or pedal position as references to the control law. Through this solution, it is possible to increase the vertical load in the main landing gear and consequently enhance braking efficiency.


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    Titel :

    USE OF AUTOMATIC PITCH CONTROL TO IMPROVE BRAKING PERFORMANCE


    Weitere Titelangaben:

    VERWENDUNG EINER AUTOMATISCHEN NICKSTEUERUNG ZUR VERBESSERUNG DER BREMSLEISTUNG
    UTILISATION DE COMMANDE AUTOMATIQUE DE TANGUAGE POUR AMÉLIORER LA PERFORMANCE DE FREINAGE



    Erscheinungsdatum :

    2020-01-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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