A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.


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    Titel :

    Display of aircraft altitude


    Beteiligte:
    VERNALEKEN CHRISTOPH (Autor:in) / OPITZ MARCO (Autor:in) / NEUJAHR HARALD (Autor:in) / FERREIRA EUGENIO (Autor:in) / BROSZIO LUTZ (Autor:in)

    Erscheinungsdatum :

    2018-06-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme



    Display of Aircraft Altitude

    VERNALEKEN CHRISTOPH / OPITZ MARCO / NEUJAHR HARALD et al. | Europäisches Patentamt | 2015

    Freier Zugriff

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