Method and system for assisting flight control of a...

Details Method and system for assisting flight control of a... Method and system for assisting flight control of a...

G - Physics

08

G

G08G 5/04 (2006.01) B64D 43/00 (2006.01) G01C 23/00 (2006.01)

Patent

CA 2611369

The system (1) comprises means (6) for determining a limit angle of climb corresponding to a climb angle of the aircraft for flying over the ground along an avoidance path and means (8) for displaying a characteristic sign representing said limit angle of climb on a display screen (9).

Le système (1) comporte des moyens (6) pour déterminer une pente limite correspondant à une pente que l'aéronef doit voler pour pouvoir survoler le terrain le long d'une trajectoire d'évitement, et des moyens (8) pour présenter, sur un écran de visualisation (9), un signe caractéristique qui représente cette pente limite.

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