Low speed turn coordination for rotary wing aircraft

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

G - Physics

05

D

G05D 1/08 (2006.01)

Patent

CA 2114551

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 low speed 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 commande de vol (21) d'hélicoptère comportant un système de commande selon un modèle d'architecture qui fournit automatiquement un signal de coordination de lacet au rotor de queue de l'hélicoptère afin de coordonner le vol de l'hélicoptère au cours d'un virage incliné à basse vitesse. Le système de commande traite l'information provenant de divers capteurs (31) pour fournir un signal de coordination de lacet à la ligne de sortie (72) vers le rotor de queue de l'hélicoptère.

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