An aircraft auxiliary display system for avoiding spatial disorientation includes a central processing unit (CPU), a sensing module, an activation display unit and an electro-optical visual unit. The CPU includes a storage unit and is electrically connected to the activation display unit. The sensing module is electrically connected to the CPU and includes a flight data sensing unit. The activation display unit is electrically connected to the electro-optical visual unit.


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    Title :

    AIRCRAFT AUXILIARY DISPLAY SYSTEM FOR AVOIDING SPATIAL DISORIENTATION


    Contributors:

    Publication date :

    2023-12-21


    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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