A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.


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    Titel :

    FULL AUTHORITY FLY-BY-WIRE PEDAL SYSTEM


    Weitere Titelangaben:

    VOLLBEFUGTES VERDRAHTETES FLUG-PEDAL-SYSTEM
    SYSTÈME DE PÉDALES DE COMMANDES DE VOL ÉLECTRIQUES AYANT PLEINE AUTORITÉ


    Beteiligte:
    BOCZAR BRUCE (Autor:in) / STILES LORREN (Autor:in) / WITIAK PETER T (Autor:in)

    Erscheinungsdatum :

    2016-03-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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