High speed turn coordination for rotary wing aircraft

Details High speed turn coordination for rotary wing aircraft High speed turn coordination for rotary wing aircraft

G - Physics

05

D

G05D 1/08 (2006.01)

Patent

CA 2116564

A helicopter flight control system (21) 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 (31) in order to provide the coordinating yaw command signal on an output line (72) to the tail rotor (20) of the helicopter.

Système de commandes de vol d'hélicoptère (21) présentant une architecture de système de commandes correspondant à un modèle et conçu pour fournir automatiquement un signal de commande de lacet de coordination au rotor anticouple de l'hélicoptère en vue de coordonner le vol de l'hélicoptère lorsqu'il effectue un virage incliné. Ce système de commandes traite les informations émises par divers capteurs (31) de l'hélicoptère pour fournir le signal de commande de lacet de coordination à son rotor anticouple (20) par l'intermédiaire d'une ligne de sortie (72).

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