The method involves correcting an instruction of braking according to a pitching angle (theta) of an aircraft (1) during braking. The correction process is carried out by subtracting the instruction of braking from a breaking setpoint correction value. The breaking setpoint correction value is calculated according to the pitching angle when the aircraft runs at a ground speed (V) with a lower threshold speed (Vseuil). The breaking setpoint correction value is set to zero when the ground speed is greater than or equal to the threshold speed.


    Access

    Download


    Export, share and cite



    Title :

    Procédé de gestion du freinage d'un aéronef permettant de limiter son tangage


    Additional title:

    Braking control method for landed airplane, aiming to optimise its pitching anle.
    Verfahren zum Steuern das Bremsen eines gelandeten Flugzeugs zur Reduzierung seines Gierwinkels.


    Contributors:

    Publication date :

    2017-08-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



    PROCEDE DE GESTION DU FREINAGE D'UN AERONEF PERMETTANT DE LIMITER SON TANGAGE

    BENMOUSSA MICHAEL | European Patent Office | 2015

    Free access

    Procédé de gestion du freinage d'un aéronef

    VANEY JEAN-BAPTISTE / FRANK DAVID / LEMAY DAVID | European Patent Office | 2018

    Free access

    PROCEDE DE GESTION DU FREINAGE D'UN AERONEF.

    VANEY JEAN-BAPTISTE / FRANK DAVID / LEMAY DAVID | European Patent Office | 2016

    Free access

    PROCEDE DE GESTION DU FREINAGE D'UN AERONEF.

    VANEY JEAN-BAPTISTE / FRANK DAVID / LEMAY DAVID | European Patent Office | 2016

    Free access

    PROCEDE DE FREINAGE SECOURS D'UN AERONEF

    FRANK DAVID / FRAVAL JEROME / WARINT DONNY | European Patent Office | 2020

    Free access