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.
AIRCRAFT AUXILIARY DISPLAY SYSTEM FOR AVOIDING SPATIAL DISORIENTATION
21.12.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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