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.
Procédé de détermination dynamique de la position du point d'arrêt d'un aéronef sur un terrain, et système associé
Method and system for dynamically determing the stopping point on ground of an aircraft
Verfahren und System zur dynamischen Bestimmen des Haltepunktes auf dem Boden von einem Flugzeug
2019-01-16
Patent
Electronic Resource
French
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