An aircraft includes a main body, a structure member, and a retroreflective member. The structure member is provided below the main body in a gravity direction. The retroreflective member is provided in the structure member and reflects a light, which is emitted from a ground facility, toward the ground facility.


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    Titel :

    AIRCRAFT AND AIRCRAFT GUIDANCE SYSTEM


    Beteiligte:
    YOSHIKAWA SATORU (Autor:in) / MATSUE TAKENORI (Autor:in) / MITSUDA TETSUJI (Autor:in) / HIRAI MASATAKA (Autor:in)

    Erscheinungsdatum :

    28.01.2021


    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 / B64C AEROPLANES , Flugzeuge / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



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