Low speed model following velocity command system for rotary...

Details Low speed model following velocity command system for rotary... Low speed model following velocity command system for rotary...

G - Physics

05

D

G05D 1/08 (2006.01) G05D 1/00 (2006.01) G05D 1/06 (2006.01)

Patent

CA 2116565

A rate model algorithm responsive to the pilot attitude command signal, flight parameters sensors and an inverse vehicle model algorithm provide signals to rotary wing aircraft flight command to get the aerodynamical response to the pilot command.

Un algorithme pour modèle de contrôle de tangage réagissant aux signaux de commande d'assiette envoyés par le pilote, des capteurs de paramètres de vol et un algorithme pour modèle inverse pour véhicule fournissent des signaux aux commandes de vol d'aéronefs à voilure tournante pour obtenir la réaction aérodynamique aux commandes de pilotage.

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