The method involves dynamically measuring a current geographical position of an aircraft (12) and its current ground speed, and calculating a length representative of a flight phase of the aircraft. Another length representative of a ground phase of the aircraft is calculated. The position of a stop point (16) of the aircraft is calculated based on the former length, the latter length and the current geographical position, where the calculation of the former length includes a phase for dynamically estimating a distance traveled by the aircraft during a part of a flare phase of the aircraft. An independent claim is also included for a system for dynamically determining the position of the stop point of an aircraft on a terrain.


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    Title :

    PROCEDE DE DETERMINATION DYNAMIQUE DE LA POSITION DU POINT D'ARRET D'UN AERONEF SUR UN TERRAIN, ET SYSTEME ASSOCIE


    Contributors:

    Publication date :

    2015-12-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS