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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creator | ANDERSON, Eric N STOVER, Keith A FANNIN, Timothy R |
description | 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. |
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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.</description><language>eng ; fre ; ger</language><subject>GYROSCOPIC INSTRUMENTS ; MEASURING ; MEASURING DISTANCES, LEVELS OR BEARINGS ; NAVIGATION ; PHOTOGRAMMETRY OR VIDEOGRAMMETRY ; PHYSICS ; SIGNALLING ; SURVEYING ; TESTING ; TRAFFIC CONTROL SYSTEMS</subject><creationdate>2021</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211208&DB=EPODOC&CC=EP&NR=3920162A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,782,887,25573,76557</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211208&DB=EPODOC&CC=EP&NR=3920162A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ANDERSON, Eric N</creatorcontrib><creatorcontrib>STOVER, Keith A</creatorcontrib><creatorcontrib>FANNIN, Timothy R</creatorcontrib><title>AIRCRAFT SYSTEM AND METHOD TO PROVIDE GRAPHICAL THRESHOLD INDICATOR</title><description>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.</description><subject>GYROSCOPIC INSTRUMENTS</subject><subject>MEASURING</subject><subject>MEASURING DISTANCES, LEVELS OR BEARINGS</subject><subject>NAVIGATION</subject><subject>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</subject><subject>PHYSICS</subject><subject>SIGNALLING</subject><subject>SURVEYING</subject><subject>TESTING</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHB29AxyDnJ0C1EIjgwOcfVVcPRzUfB1DfHwd1EI8VcICPIP83RxVXAPcgzw8HR29FEI8QhyDfbw93FR8PRzAYqE-AfxMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JJ41wBjSyMDQzMjR0NjIpQAANm6KxY</recordid><startdate>20211208</startdate><enddate>20211208</enddate><creator>ANDERSON, Eric N</creator><creator>STOVER, Keith A</creator><creator>FANNIN, Timothy R</creator><scope>EVB</scope></search><sort><creationdate>20211208</creationdate><title>AIRCRAFT SYSTEM AND METHOD TO PROVIDE GRAPHICAL THRESHOLD INDICATOR</title><author>ANDERSON, Eric N ; STOVER, Keith A ; FANNIN, Timothy R</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3920162A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><topic>GYROSCOPIC INSTRUMENTS</topic><topic>MEASURING</topic><topic>MEASURING DISTANCES, LEVELS OR BEARINGS</topic><topic>NAVIGATION</topic><topic>PHOTOGRAMMETRY OR VIDEOGRAMMETRY</topic><topic>PHYSICS</topic><topic>SIGNALLING</topic><topic>SURVEYING</topic><topic>TESTING</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><toplevel>online_resources</toplevel><creatorcontrib>ANDERSON, Eric N</creatorcontrib><creatorcontrib>STOVER, Keith A</creatorcontrib><creatorcontrib>FANNIN, Timothy R</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ANDERSON, Eric N</au><au>STOVER, Keith A</au><au>FANNIN, Timothy R</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT SYSTEM AND METHOD TO PROVIDE GRAPHICAL THRESHOLD INDICATOR</title><date>2021-12-08</date><risdate>2021</risdate><abstract>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.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SIGNALLING SURVEYING TESTING TRAFFIC CONTROL SYSTEMS |
title | AIRCRAFT SYSTEM AND METHOD TO PROVIDE GRAPHICAL THRESHOLD INDICATOR |
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