G - Physics – 01 – C
Patent
G - Physics
01
C
G01C 21/00 (2006.01) B64D 45/00 (2006.01) G01C 23/00 (2006.01)
Patent
CA 2611984
A device comprises means for computing the aircraft (A) current position, means for determining at least one maximum permitted deviation (E1) around a set position of the flight path of the flight plan according to accuracy and integrity performances of said current position computation and to the restriction of a flight range authorised in a flight corridor (6A, 6B), and a display system (7) for displaying at least one a distance scale (9) on a viewing screen (8), at least one fixed symbol (10) displaying the current position and two movable pointers (13, 14) displaying the limits of said maximum permitted deviation (E1).
Procédé et dispositif d'affichage pour un aéronef qui suit un plan de vol. Le dispositif comporte un moyen pour calculer la position effective de l'aéronef (A), un moyen pour déterminer au moins un écart maximal autorisé (E1) autour d'une position de consigne sur une trajectoire de vol (5) issue du plan de vol, en fonction de performances de précision et d'intégrité de calcul de ladite position effective et d'une contrainte de zone de vol autorisée dans un couloir de vol (6A, 6B), et un système d'affichage (7) pour présenter sur un écran de visualisation (8), au moins une échelle de distance (9), au moins un symbole fixe (10) qui indique ladite position effective, et deux indicateurs mobiles (13, 14) qui indiquent les limites (15A, 15B) dudit écart maximal autorisé (E1).
Have Didier
Laveant Nolween
Le Tellier Arnaud
Rouquette Patrice
Airbus France
Airbus Operations Sas
Robic
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