SYSTEMS AND METHODS FOR DYNAMIC LIGHT CONTROL

A light system for an aircraft is provided. A light system may include a sensor (90) and a first aircraft light (22). A controller (110) may be coupled to the sensor and the first aircraft light and may perform operations including receiving data from the sensor, determining a status of the aircraft...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KELLER, Steven T, HESSLING VON HEIMENDAHL, Andre
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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