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.


    Access

    Download


    Export, share and cite



    Title :

    AVIATION SYSTEM AND AVIATION METHOD


    Additional title:

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


    Contributors:

    Publication date :

    2024-01-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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




    Aviation : aviation maintenance

    English Language Services | TIBKAT | 1984


    AVIATION SYSTEM

    TSUBATA HIROYUKI / MIYAKI HIROMITSU / OKADA TAKAO | European Patent Office | 2022

    Free access

    VERTICAL TAKEOFF AND LANDING-DEDICATED AVIATION LIGHTING, AVIATION LIGHTING SYSTEM, AND AVIATION LIGHTING METHOD

    KOH DONGHEE / JUNG MINCHUL / YU KEUMSIK et al. | European Patent Office | 2025

    Free access