Method and system for limiting an aircraft control surface...

Details Method and system for limiting an aircraft control surface... Method and system for limiting an aircraft control surface...

G - Physics

05

D

G05D 1/00 (2006.01)

Patent

CA 2625747

The invention concerns a method for limiting an aircraft control surface steering angle, including the following operations: determining a maximum authorized steering angle based on the aircraft speed, detecting a side-slip configuration of the aircraft followed by a first steering control of the control surface with a maximum steering angle and in a first direction, applying a limitation of the maximum authorized steering angle. The invention also concerns a device for implementing said method.

L'invention concerne un procédé de limitation de l'angle de braquage d'une gouverne d'un aéronef, comportant les opérations de - détermination d'un angle de braquage maximum autorisé en fonction de la vitesse de l'aéronef, - détection d'une configuration de dérapage de l'aéronef suivie d'une première commande de braquage de la gouverne avec un angle de braquage maximum et un premier sens, - application d'une limitation de l'angle de braquage maximum autorisé. L'invention concerne également un système pour mettre en AEuvre ce procédé.

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