According to one embodiment, a flying object monitoring system comprises a reception unit which receives flight information of a flying object, a calculation unit which calculates acceleration in each flight direction of the flying object from the flight information, a representation unit which represents the calculated acceleration with an acceleration distribution image formed by plotting the calculated acceleration with respect to the flight direction, and a determination unit which determines whether the flying object is malfunctioning based on the acceleration distribution image.


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    Title :

    FLYING OBJECT MONITORING SYSTEM


    Contributors:

    Publication date :

    2025-03-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01S RADIO DIRECTION-FINDING , Funkpeilung



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