A flight hindrance display apparatus includes circuitry. The circuitry is configured to acquire surrounding information of an aircraft. The surrounding information is related to the a hindrance factor which is a possible flight hindrance to the aircraft. The circuitry is configured to determine a spatial range of the flight hindrance factor on a basis of the acquired surrounding information. The circuitry is configured to determine a flight hindrance cross-section that intersects a plane including a vector of a flight direction of the aircraft and is included in the determined spatial range of the flight hindrance factor. The circuitry is configured to cause a display unit to stereoscopically display an own position of the aircraft, the spatial range of the flight hindrance factor, and the flight hindrance cross-section.


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    Titel :

    FLIGHT HINDRANCE DISPLAY APPARATUS, FLIGHT HINDRANCE DISPLAY METHOD, AND COMPUTER-READABLE MEDIUM


    Beteiligte:
    ONOMURA YOICHI (Autor:in) / TAKAHASHI SHINEI (Autor:in) / ITABASHI YU (Autor:in)

    Erscheinungsdatum :

    2017-09-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / G01S RADIO DIRECTION-FINDING , Funkpeilung / H04N PICTORIAL COMMUNICATION, e.g. TELEVISION , Bildübertragung, z.B. Fernsehen



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