In the method according to the invention, when the head support is oriented in a determined direction making, with the horizon line and/or with the “speed vector”, an angle greater than a first value, and/or when at least one of the attitude parameters of the aircraft becomes greater than a second value, the attitude director indicator is displayed locally in a reference frame tied to the head support and in the field of the viewing device.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    METHOD OF DISPLAYING AN "ATTITUDE DIRECTOR INDICATOR" IN A HEAD VIEWING SYSTEM FOR AIRCRAFT


    Beteiligte:
    SACHEAU ROMAIN (Autor:in) / AYMERIC BRUNO (Autor:in) / BARREAU JONATHAN (Autor:in)

    Erscheinungsdatum :

    2017-06-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft attitude indicator device

    LAINE FRANCK / SAPIN OLIVIER / RENAULT LEBERQUER CHARLES | Europäisches Patentamt | 2017

    Freier Zugriff


    AIRCRAFT ATTITUDE INDICATOR DEVICE

    LAINE FRANCK / SAPIN OLIVIER / RENAULT LEBERQUER CHARLES | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT CAMERA VIEWING SYSTEM

    DE BOER DYLAN / DE BOER ANTHONY | Europäisches Patentamt | 2018

    Freier Zugriff

    INTUITIVE DISPLAY OF ANGLE OF ATTACK GUIDANCE ON AIRCRAFT ATTITUDE INDICATOR

    WATSON GARY | Europäisches Patentamt | 2018

    Freier Zugriff