High speed yaw control system for rotary wing aircraft

Details High speed yaw control system for rotary wing aircraft High speed yaw control system for rotary wing aircraft

G - Physics

05

D

G05D 1/08 (2006.01) B64C 13/50 (2006.01) G05D 1/00 (2006.01)

Patent

CA 2113730

A helicopter flight control system includes a model following control system architecture which automatically provides a coordinating yaw command signal to the helicopter tail rotor to coordinate helicopter flight during a banked turn. The control system processes information from a variety of helicopter sensors in order to provide the coordinating yaw command signal on an output line to the tail rotor of the helicopter.

Système de commande de vol pour hélicoptère comportant une architecture de système de commande fondée sur un modèle qui fournit automatiquement un signal coordinateur de commande de lacet au rotor arrière de l'hélicoptère afin de coordonner le vol de l'hélicoptère pendant un virage incliné. Ledit système de commande traite les informations provenant d'une série de capteurs situés sur l'hélicoptère afin de fournir le signal de commande de lacet coordinateur sur une ligne de sortie au rotor arrière de l'hélicoptère.

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