An embodiment aircraft includes an aircraft body including a fuselage, a status information detection device disposed in or on the aircraft body, a controller disposed in or on the aircraft body and configured to determine whether an emergency landing situation exists based on aircraft status information detected by the status information detection device and, in response to a determination that the emergency landing situation exists, calculate an expected emergency landing point, and an external output device disposed in or on the aircraft body and configured to output warning information toward the expected emergency landing point, wherein the warning information includes a sound or a light.


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    Title :

    AIRCRAFT WITH EMERGENCY LANDING POINT WARNING SYSTEM


    Contributors:

    Publication date :

    2025-06-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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