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.


    Access

    Download


    Export, share and cite



    Title :

    PROCEDE D'AFFICHAGE D'UN "INDICATEUR DE DIRECTEUR D'ATTITUDE" DANS UN SYSTEME DE VISUALISATION DE TETE POUR AERONEF


    Contributors:

    Publication date :

    2017-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    G02B Optische Elemente, Systeme oder Geräte , OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    DISPOSITIF INDICATEUR D'ATTITUDE D'UN AERONEF

    LAINE FRANCK / SAPIN OLIVIER / RENAULT LEBERQUER CHARLES | European Patent Office | 2017

    Free access

    SYSTEME ET PROCEDE D'AFFICHAGE D'UN AERONEF

    DESCHEEMAEKER CEDRIC / MANJON SANCHEZ JAVIER | European Patent Office | 2017

    Free access

    SYSTEME ET PROCEDE D'AFFICHAGE D'UN AERONEF

    PERRIN AYMERIC / CHARBONNIER CHRISTINE / ANTONI NICOLAS et al. | European Patent Office | 2017

    Free access

    PROCEDE ET DISPOSITIF D’AFFICHAGE D’AU MOINS UN INDICATEUR DE POSITION D’UN AERONEF.

    CROSTA FRANCK / CAIL CHRISTOPHE | European Patent Office | 2019

    Free access

    SYSTEME ET PROCEDE D'AFFICHAGE POUR UN AERONEF

    MANJON SANCHEZ JAVIER / DESCHEEMAEKER CEDRIC | European Patent Office | 2019

    Free access