G - Physics – 05 – D
Patent
G - Physics
05
D
G05D 1/00 (2006.01) B64D 45/04 (2006.01) G05D 1/06 (2006.01)
Patent
CA 2640184
Method and system for predicting the possibility of complete stoppage of an aircraft on a landing runway. According to the invention: a) the altitude (H) of the aircraft (2) is measured and the horizontal distance (D) separating said aircraft (2) from the proximal end threshold (4) of the landing runway (1) is calculated; b) an estimated finishing position (21) of said aircraft on said landing runway (1) is calculated on the basis of the altitude (H) and of the horizontal distance (D) determined in a), as well as on the basis of the angle of approach (.alpha.); and c) said estimated finishing position (21) calculated in b) is utilized to determine said possibility.
Procédé et système pour prédire la possibilité d'arrêt complet d'un aéronef sur une piste d'atterrissage. Selon l'invention : a) on mesure l'altitude (H) de l'aéronef (2) et on calcule la distance horizontale (D) séparant ledit aéronef (2) du seuil d'extrémité proximal (4) de la piste d'atterrissage (1 ) ; b) on calcule, à partir de l'altitude (H) et de la distance horizontale (D) déterminées sous a), ainsi qu'à partir de l'angle d'approche (.alpha.), une position d'aboutissement estimée (21 ) dudit aéronef sur ladite piste d'atterrissage (1 ) ; et c) on exploite ladite position d'aboutissement estimée (21 ) calculée sous b) pour déterminer ladite possibilité.
Airbus France
Airbus Operations Sas
Robic
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