Automatic turn coordination trim control for rotary wing...

Details Automatic turn coordination trim control for rotary wing... Automatic turn coordination trim control for rotary wing...

G - Physics

05

D

G05D 1/08 (2006.01)

Patent

CA 2113731

A helicopter flight control system includes an automatic turn coordination system which provides a coordinating yaw command signal to the tail rotor of the helicopter. The system stores on command a trim attitude (e.g., signals indicative of bank angle, lateral ground speed, and lateral acceleration) about which automatic turn coordination is provided, thus providing the pilot with automatic turn coordination about attitudes other than wings level.

Système de commande de vol pour hélicoptère comportant un système de coordination automatique de virage qui fournit un signal coordinateur de commande de lacet au rotor arrère de l'hélicoptère. Sur commande, le système met en mémoire une assiette (par ex., signaux indicateurs de l'angle d'inclinaison latérale, vitesse au sol latérale et accélération latérale) qui permet de fournir une coordination automatique de virage, donnant ainsi au pilote une coordination automatique de virage sur des assiettes autre que celle où l'aéronefs reste horizontal.

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