AIRCRAFT SYSTEM AND METHOD TO PROVIDE GRAPHICAL THRESHOLD INDICATOR

A system may (100) include a display (302) and a processor (202). The display (302) may be configured to present images to a user, the display (302) in an ownship. The processor (202) may be communicatively coupled to the display (302) and in the ownship. The processor (202) may be configured to: re...

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Bibliographische Detailangaben
Hauptverfasser:	ANDERSON, Eric N, STOVER, Keith A, FANNIN, Timothy R
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SIGNALLING SURVEYING TESTING TRAFFIC CONTROL SYSTEMS
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Beschreibung
Zusammenfassung:	A system may (100) include a display (302) and a processor (202). The display (302) may be configured to present images to a user, the display (302) in an ownship. The processor (202) may be communicatively coupled to the display (302) and in the ownship. The processor (202) may be configured to: receive aircraft traffic data and ownship data; at least one of determine or adjust a threshold range based at least on the aircraft traffic data and the ownship data, the threshold range representing a time or distance threshold to designated traffic; generate and update a graphical threshold indicator, the threshold indicator representing a time or distance from the threshold range to the designated traffic; and output the graphical threshold indicator as graphical data to the display. The display (302) may be configured to display the graphical threshold indicator to the user.