MULTI-DIMENSIONAL AIRCRAFT COLLISION CONFLICT RISK EVALUATION SYSTEM
A multi-dimensional aircraft collision conflict risk evaluation system in the field of civil aviation aircraft collision conflict prediction. The system executes the steps of: S1, calculating probabilities that an aircraft overlaps other aircrafts in three dimensions; S2, calculating loss interval r...
Gespeichert in:
Hauptverfasser: | , , , , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng ; fre |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | WANG, Xuan WANG, Siyu CHEN, Kuanming ZHANG, Xiaolei LIAN, Jingyu PAN, Weijun CHEN, Jiayang |
description | A multi-dimensional aircraft collision conflict risk evaluation system in the field of civil aviation aircraft collision conflict prediction. The system executes the steps of: S1, calculating probabilities that an aircraft overlaps other aircrafts in three dimensions; S2, calculating loss interval rates of the aircraft in the three dimensions; S3, obtaining probabilities that the aircraft conflicts and collides with the other aircrafts in three dimensional directions; S4, comparing the probabilities that the aircraft conflicts and collides in the three dimensional directions to obtain a maximum probability and a dimension corresponding to the maximum probability; and S5, performing difference value calculation on the obtained maximum probability and a safety standard, and giving safety evaluation according to a difference value. Therefore, multi-dimensional calculation of the collision conflict risk probability of the aircraft is implemented. The maximum value of the collision conflict risk probability is obt |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_WO2021196504A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>WO2021196504A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_WO2021196504A13</originalsourceid><addsrcrecordid>eNrjZHDxDfUJ8dR18fR19Qv29Pdz9FFw9AxyDnJ0C1Fw9vfx8QQJAll-bj6eziEKQZ7B3gquYY4-oY4hIIngyOAQV18eBta0xJziVF4ozc2g7OYa4uyhm1qQH59aXJCYnJqXWhIf7m9kYGRoaGlmamDiaGhMnCoAP2ktIg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>MULTI-DIMENSIONAL AIRCRAFT COLLISION CONFLICT RISK EVALUATION SYSTEM</title><source>esp@cenet</source><creator>WANG, Xuan ; WANG, Siyu ; CHEN, Kuanming ; ZHANG, Xiaolei ; LIAN, Jingyu ; PAN, Weijun ; CHEN, Jiayang</creator><creatorcontrib>WANG, Xuan ; WANG, Siyu ; CHEN, Kuanming ; ZHANG, Xiaolei ; LIAN, Jingyu ; PAN, Weijun ; CHEN, Jiayang</creatorcontrib><description>A multi-dimensional aircraft collision conflict risk evaluation system in the field of civil aviation aircraft collision conflict prediction. The system executes the steps of: S1, calculating probabilities that an aircraft overlaps other aircrafts in three dimensions; S2, calculating loss interval rates of the aircraft in the three dimensions; S3, obtaining probabilities that the aircraft conflicts and collides with the other aircrafts in three dimensional directions; S4, comparing the probabilities that the aircraft conflicts and collides in the three dimensional directions to obtain a maximum probability and a dimension corresponding to the maximum probability; and S5, performing difference value calculation on the obtained maximum probability and a safety standard, and giving safety evaluation according to a difference value. Therefore, multi-dimensional calculation of the collision conflict risk probability of the aircraft is implemented. The maximum value of the collision conflict risk probability is obt</description><language>chi ; eng ; fre</language><subject>CALCULATING ; COMPUTING ; COUNTING ; ELECTRIC DIGITAL DATA PROCESSING ; PHYSICS ; SIGNALLING ; 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=20211007&DB=EPODOC&CC=WO&NR=2021196504A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211007&DB=EPODOC&CC=WO&NR=2021196504A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WANG, Xuan</creatorcontrib><creatorcontrib>WANG, Siyu</creatorcontrib><creatorcontrib>CHEN, Kuanming</creatorcontrib><creatorcontrib>ZHANG, Xiaolei</creatorcontrib><creatorcontrib>LIAN, Jingyu</creatorcontrib><creatorcontrib>PAN, Weijun</creatorcontrib><creatorcontrib>CHEN, Jiayang</creatorcontrib><title>MULTI-DIMENSIONAL AIRCRAFT COLLISION CONFLICT RISK EVALUATION SYSTEM</title><description>A multi-dimensional aircraft collision conflict risk evaluation system in the field of civil aviation aircraft collision conflict prediction. The system executes the steps of: S1, calculating probabilities that an aircraft overlaps other aircrafts in three dimensions; S2, calculating loss interval rates of the aircraft in the three dimensions; S3, obtaining probabilities that the aircraft conflicts and collides with the other aircrafts in three dimensional directions; S4, comparing the probabilities that the aircraft conflicts and collides in the three dimensional directions to obtain a maximum probability and a dimension corresponding to the maximum probability; and S5, performing difference value calculation on the obtained maximum probability and a safety standard, and giving safety evaluation according to a difference value. Therefore, multi-dimensional calculation of the collision conflict risk probability of the aircraft is implemented. The maximum value of the collision conflict risk probability is obt</description><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>PHYSICS</subject><subject>SIGNALLING</subject><subject>TRAFFIC CONTROL SYSTEMS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHDxDfUJ8dR18fR19Qv29Pdz9FFw9AxyDnJ0C1Fw9vfx8QQJAll-bj6eziEKQZ7B3gquYY4-oY4hIIngyOAQV18eBta0xJziVF4ozc2g7OYa4uyhm1qQH59aXJCYnJqXWhIf7m9kYGRoaGlmamDiaGhMnCoAP2ktIg</recordid><startdate>20211007</startdate><enddate>20211007</enddate><creator>WANG, Xuan</creator><creator>WANG, Siyu</creator><creator>CHEN, Kuanming</creator><creator>ZHANG, Xiaolei</creator><creator>LIAN, Jingyu</creator><creator>PAN, Weijun</creator><creator>CHEN, Jiayang</creator><scope>EVB</scope></search><sort><creationdate>20211007</creationdate><title>MULTI-DIMENSIONAL AIRCRAFT COLLISION CONFLICT RISK EVALUATION SYSTEM</title><author>WANG, Xuan ; WANG, Siyu ; CHEN, Kuanming ; ZHANG, Xiaolei ; LIAN, Jingyu ; PAN, Weijun ; CHEN, Jiayang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2021196504A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng ; fre</language><creationdate>2021</creationdate><topic>CALCULATING</topic><topic>COMPUTING</topic><topic>COUNTING</topic><topic>ELECTRIC DIGITAL DATA PROCESSING</topic><topic>PHYSICS</topic><topic>SIGNALLING</topic><topic>TRAFFIC CONTROL SYSTEMS</topic><toplevel>online_resources</toplevel><creatorcontrib>WANG, Xuan</creatorcontrib><creatorcontrib>WANG, Siyu</creatorcontrib><creatorcontrib>CHEN, Kuanming</creatorcontrib><creatorcontrib>ZHANG, Xiaolei</creatorcontrib><creatorcontrib>LIAN, Jingyu</creatorcontrib><creatorcontrib>PAN, Weijun</creatorcontrib><creatorcontrib>CHEN, Jiayang</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WANG, Xuan</au><au>WANG, Siyu</au><au>CHEN, Kuanming</au><au>ZHANG, Xiaolei</au><au>LIAN, Jingyu</au><au>PAN, Weijun</au><au>CHEN, Jiayang</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MULTI-DIMENSIONAL AIRCRAFT COLLISION CONFLICT RISK EVALUATION SYSTEM</title><date>2021-10-07</date><risdate>2021</risdate><abstract>A multi-dimensional aircraft collision conflict risk evaluation system in the field of civil aviation aircraft collision conflict prediction. The system executes the steps of: S1, calculating probabilities that an aircraft overlaps other aircrafts in three dimensions; S2, calculating loss interval rates of the aircraft in the three dimensions; S3, obtaining probabilities that the aircraft conflicts and collides with the other aircrafts in three dimensional directions; S4, comparing the probabilities that the aircraft conflicts and collides in the three dimensional directions to obtain a maximum probability and a dimension corresponding to the maximum probability; and S5, performing difference value calculation on the obtained maximum probability and a safety standard, and giving safety evaluation according to a difference value. Therefore, multi-dimensional calculation of the collision conflict risk probability of the aircraft is implemented. The maximum value of the collision conflict risk probability is obt</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | chi ; eng ; fre |
recordid | cdi_epo_espacenet_WO2021196504A1 |
source | esp@cenet |
subjects | CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS SIGNALLING TRAFFIC CONTROL SYSTEMS |
title | MULTI-DIMENSIONAL AIRCRAFT COLLISION CONFLICT RISK EVALUATION SYSTEM |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-27T16%3A04%3A05IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=WANG,%20Xuan&rft.date=2021-10-07&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EWO2021196504A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |