Method and device for assisting an aircraft flight control...

G - Physics – 01 – C

Patent

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G01C 23/00 (2006.01) B64D 45/04 (2006.01) G05D 1/06 (2006.01) G08G 5/02 (2006.01)

Patent

CA 2606821

The inventive flight controll assisting device comprises first means (4) for determining the actual aircraft flight conditions, second means (5) for determining, with the aid of said actual flight conditions and a predetermined pattern, a minimum approaching distance corresponding to a minimum distance between projections on the horizontal plane of the aircraft actual position and a touch-down point when said aircraft moves downwards and decelerates according to an optimised approach in such a way that stabilised approaching conditions are attained, and display means (7) for displaying at least said minimum approaching distance on a navigation screen (9) in the form of a first circular arc focused on a position relative to the aircraft which displays the touch-down position.

Le dispositif d'aide au pilotage comporte des premiers moyens (4) pour déterminer des conditions de vol courantes de l'avion, des seconds moyens (5) pour déterminer, à l'aide desdites conditions de vol couran¬ tes et d'un modèle prédéterminé, une distance d'approche minimale qui correspond à une distance minimale entre des projections sur un plan horizontal de la position actuelle de l'avion et d'une position de contact avec le sol, lorsque l'avion descend et décélère conformément à une approche optimisée pour atteindre des conditions d'approche stabilisée, et des moyens d'affichage (7) pour présenter, sur un écran de naviga¬ tion (9), au moins cette distance d'approche minimale sous forme d'un premier arc de cercle qui est centré sur une position relative à l'avion et qui illustre la position de contact avec le sol.

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