According to one embodiment, an aviation system 100 includes electric field sensors 112 and a ground system 114 including a computer configured to communicate with each of the electric field sensors 112. The computer is configured to: acquire electric field intensities from the electric field sensors 112 respectively, and generate a first electric field distribution on a ground surface 16 based on the electric field intensities; derive a matrix; derive a pseudo inverse matrix of the matrix; derive an electric charge distribution on the horizontal plane by multiplying the pseudo inverse matrix by the first electric field distribution on the ground surface 16; and derive a second electric field distribution on a flight path based on the electric charge distribution. The first electric field distribution on the ground surface 16 is derived by multiplying the matrix by electric charges temporarily set on a horizontal plane at a predetermined altitude.


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    Titel :

    AVIATION SYSTEM AND AVIATION METHOD


    Weitere Titelangaben:

    LUFTFAHRTSYSTEM UND LUFTFAHRTVERFAHREN
    SYSTÈME D'AVIATION ET PROCÉDÉ D'AVIATION


    Beteiligte:
    TSUBATA HIROYUKI (Autor:in) / MIYAKI HIROMITSU (Autor:in) / OKADA TAKAO (Autor:in)

    Erscheinungsdatum :

    2024-01-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01W METEOROLOGY , Meteorologie



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