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...

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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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Beschreibung
Zusammenfassung:	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 based on the data, and controlling the first aircraft light based on the status of the aircraft. The first aircraft light may include an external aircraft light and the operations may further include at least one of activating or deactivating the external aircraft light based on the status of the aircraft.