Aircraft guidance system

Details Aircraft guidance system Aircraft guidance system

G - Physics

01

C

G01C 23/00 (2006.01)

Patent

CA 2641143

The guidance system (1) comprises means (2, 6) for generating an alphanumeric identification characteristic, making it possible to identify a data item which must be used for a selected guidance mode of the aircraft, and display means (10) which automatically show this alphanumeric identification characteristic on a display screen (12).

Le système de guidage (1 ) comporte des moyens (2, 6) pour engendrer une caractéristique d'identification alphanumérique, permettant d'identifier une donnée qui doit être utilisée pour un mode de guidage sélectionné de l'aéronef, et des moyens d'affichage (10) qui présentent automatiquement cette caractéristique d'identification alphanumérique sur un écran de visualisation (12).

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