Method and device for assisted flight management of an aircraft during a landing phase

The method involves receiving information relative to actual conditions regarding an environment and a runway (15), and determining a maximum shift (Dmax) corresponding to the maximum longitudinal shift along the runway. Predetermined criteria and the maximum shift are determined, where an actual sh...

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Bibliographic Details
Main Authors DUMOULIN, ANNE, LOCHERON, MARC
Format Patent
LanguageEnglish
French
German
Published 13.11.2013
Subjects
CONTROLLING
PHYSICS
REGULATING
SIGNALLING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRAFFIC CONTROL SYSTEMS
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Summary:The method involves receiving information relative to actual conditions regarding an environment and a runway (15), and determining a maximum shift (Dmax) corresponding to the maximum longitudinal shift along the runway. Predetermined criteria and the maximum shift are determined, where an actual shift (Deff) is less than the maximum shift. A shift point (P0f) is shifted from a threshold of the runway along a downstream direction. An adaptive aiming point (P1f) is calculated from the shift point. The adaptive aiming point is transmitted to a landing aid unit of an aircraft. An independent claim is also included for a device for assisting flight management of an aircraft during a landing phase. - Procédé et dispositif d'aide à la gestion du vol d'un aéronef lors d'une phase d'atterrissage. - Le dispositif comporte des moyens pour déterminer automatiquement un point d'aboutissement adapté (P1f) qui est décalé le long de la piste d'atterrissage (15) vers l'aval et qui peut être utilisé par différents moyens usuels d'aide à l'atterrissage de l'aéronef.
Bibliography:Application Number: EP20130165026