Method and system for piloting an aircraft

G - Physics – 05 – D

Patent

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G05D 1/06 (2006.01)

Patent

CA 2637689

The invention concerns a system (1) comprising guiding means (3) which, when guiding the aircraft along a low-altitude flight path, and upon a climb command, continue guiding the aircraft along the lateral path of said low-altitude flight path, and subject the aircraft in the vertical plane to a climb along a climb gradient which is not less than a maximum gradient of said flight path.

Le système (1) comporte des moyens de guidage (3) qui, lorsqu'ils guident l'aéronef le long d'une trajectoire de vol à basse hauteur, et qu'une montée est commandée, continuent à guider l'aéronef le long de la trajectoire latérale de cette trajectoire de vol à basse hauteur dans le plan horizontal, et soumettent l'aéronef dans le plan vertical à une montée selon une pente de montée qui est supérieure ou égale à une pente maximale sur ladite trajectoire de vol.

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