The device (1) has an automatic brake (10) that is utilized to automatically slow down an aircraft i.e. civil transport aircraft, in a landing strip or runway, and a data providing unit (12) for providing data having a high level of integrity. A calculating unit (13) is utilized to calculate minimal deceleration. A comparison unit (14) compares nominal deceleration with minimal deceleration, and highest deceleration value is transmitted to a controller (7). The calculating unit and the comparison unit are provided as a part of another controller (4). An independent claim is also included for a method for assisting piloting of an aircraft.


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    Title :

    Procédé et dispositif d'aide au pilotage d'un avion lors d'une phase d'atterrissage


    Additional title:

    Method and device for assisted piloting of an aircraft during a landing phase
    Verfahren und Vorrichtung zur Unterstützung der Steuerung eines Flugzeugs in der Landephase


    Contributors:

    Publication date :

    2016-12-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    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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