Orbit determination of medium-high earth orbital satellite using GNSS crosslink ranging observations

Precise orbit determination of medium and high earth orbital satellites mainly depends on ground-based tracking systems, which have limitations such as insufficient tracking arc, low accuracy, and are often unable to support autonomous navigation. The foundation of a GNSS crosslink network provides...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Geomatics and Information Science of Wuhan University 2014-04, Vol.39 (4), p.445-449
Hauptverfasser: Meng, Yinan, Fan, Shiwei, Li, Gang, Gao, Weiguang
Format: Artikel
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 449
container_issue 4
container_start_page 445
container_title Geomatics and Information Science of Wuhan University
container_volume 39
creator Meng, Yinan
Fan, Shiwei
Li, Gang
Gao, Weiguang
description Precise orbit determination of medium and high earth orbital satellites mainly depends on ground-based tracking systems, which have limitations such as insufficient tracking arc, low accuracy, and are often unable to support autonomous navigation. The foundation of a GNSS crosslink network provides a new resolution for orbit determination of medium and high earth orbital satellites. This paper introduces a new method, used for orbit determination of medium and high earth orbital satellites based on GNSS crosslink ranging observations. The visibility, positioning accuracy, and crosslink budget has been analyzed and the simulative calculation of Autonomous Orbit Determination (AOD) was performed. The results show that with sufficient visible satellite numbers, positioning accuracy, and link margins, the AOD of medium-high earth orbital satellites using GNSS crosslink ranging observations can achieve a positioning error within 6 m in radial, 2 m along and across; the new method is feasible and can open new directions in the application of GNSS.
doi_str_mv 10.13203/j.whugis20120215
format Article
fullrecord <record><control><sourceid>proquest</sourceid><recordid>TN_cdi_proquest_miscellaneous_1701104843</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>1541418821</sourcerecordid><originalsourceid>FETCH-LOGICAL-p136t-6c18a40518fdff71630c3894d32b3512e86bf4c844a9bb7c5eb1d3ba15c2d14b3</originalsourceid><addsrcrecordid>eNqFjrtOwzAYRj2ARFX6AGweWVL8-xZ3RBUUpIoOhbnyLYkhiYvtwOtDgZ3pk46Ojj6EroAsgVHCbl6Xn93UhkwJUEJBnKEZyBoqpSS5QIucgyFMcsYpFTPkdsmEgp0vPg1h1CXEEccGD96Faai60HbY61Q6HE-i7nHWxfd9KB5POYwt3jzt99immHMfxjec9NiecDTZp4-fXr5E543us1_87Ry93N89rx-q7W7zuL7dVkdgslTSgtKcCFCNa5oaJCOWqRV3jBomgHolTcOt4lyvjKmt8AYcMxqEpQ64YXN0_ds9pvg--VwOQ8j2-60efZzyAWoCQLji7H9VcOCgFAX2BcIXaaY</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1541418821</pqid></control><display><type>article</type><title>Orbit determination of medium-high earth orbital satellite using GNSS crosslink ranging observations</title><source>Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals</source><creator>Meng, Yinan ; Fan, Shiwei ; Li, Gang ; Gao, Weiguang</creator><creatorcontrib>Meng, Yinan ; Fan, Shiwei ; Li, Gang ; Gao, Weiguang</creatorcontrib><description>Precise orbit determination of medium and high earth orbital satellites mainly depends on ground-based tracking systems, which have limitations such as insufficient tracking arc, low accuracy, and are often unable to support autonomous navigation. The foundation of a GNSS crosslink network provides a new resolution for orbit determination of medium and high earth orbital satellites. This paper introduces a new method, used for orbit determination of medium and high earth orbital satellites based on GNSS crosslink ranging observations. The visibility, positioning accuracy, and crosslink budget has been analyzed and the simulative calculation of Autonomous Orbit Determination (AOD) was performed. The results show that with sufficient visible satellite numbers, positioning accuracy, and link margins, the AOD of medium-high earth orbital satellites using GNSS crosslink ranging observations can achieve a positioning error within 6 m in radial, 2 m along and across; the new method is feasible and can open new directions in the application of GNSS.</description><identifier>ISSN: 1671-8860</identifier><identifier>DOI: 10.13203/j.whugis20120215</identifier><language>chi ; eng</language><subject>Argon oxygen decarburizing ; Autonomous ; Crosslinking ; Earth orbital environments ; GNSS ; Orbit determination ; Satellite tracking ; Satellites</subject><ispartof>Geomatics and Information Science of Wuhan University, 2014-04, Vol.39 (4), p.445-449</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,777,781,27905,27906</link.rule.ids></links><search><creatorcontrib>Meng, Yinan</creatorcontrib><creatorcontrib>Fan, Shiwei</creatorcontrib><creatorcontrib>Li, Gang</creatorcontrib><creatorcontrib>Gao, Weiguang</creatorcontrib><title>Orbit determination of medium-high earth orbital satellite using GNSS crosslink ranging observations</title><title>Geomatics and Information Science of Wuhan University</title><description>Precise orbit determination of medium and high earth orbital satellites mainly depends on ground-based tracking systems, which have limitations such as insufficient tracking arc, low accuracy, and are often unable to support autonomous navigation. The foundation of a GNSS crosslink network provides a new resolution for orbit determination of medium and high earth orbital satellites. This paper introduces a new method, used for orbit determination of medium and high earth orbital satellites based on GNSS crosslink ranging observations. The visibility, positioning accuracy, and crosslink budget has been analyzed and the simulative calculation of Autonomous Orbit Determination (AOD) was performed. The results show that with sufficient visible satellite numbers, positioning accuracy, and link margins, the AOD of medium-high earth orbital satellites using GNSS crosslink ranging observations can achieve a positioning error within 6 m in radial, 2 m along and across; the new method is feasible and can open new directions in the application of GNSS.</description><subject>Argon oxygen decarburizing</subject><subject>Autonomous</subject><subject>Crosslinking</subject><subject>Earth orbital environments</subject><subject>GNSS</subject><subject>Orbit determination</subject><subject>Satellite tracking</subject><subject>Satellites</subject><issn>1671-8860</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNqFjrtOwzAYRj2ARFX6AGweWVL8-xZ3RBUUpIoOhbnyLYkhiYvtwOtDgZ3pk46Ojj6EroAsgVHCbl6Xn93UhkwJUEJBnKEZyBoqpSS5QIucgyFMcsYpFTPkdsmEgp0vPg1h1CXEEccGD96Faai60HbY61Q6HE-i7nHWxfd9KB5POYwt3jzt99immHMfxjec9NiecDTZp4-fXr5E543us1_87Ry93N89rx-q7W7zuL7dVkdgslTSgtKcCFCNa5oaJCOWqRV3jBomgHolTcOt4lyvjKmt8AYcMxqEpQ64YXN0_ds9pvg--VwOQ8j2-60efZzyAWoCQLji7H9VcOCgFAX2BcIXaaY</recordid><startdate>20140401</startdate><enddate>20140401</enddate><creator>Meng, Yinan</creator><creator>Fan, Shiwei</creator><creator>Li, Gang</creator><creator>Gao, Weiguang</creator><scope>7SP</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope></search><sort><creationdate>20140401</creationdate><title>Orbit determination of medium-high earth orbital satellite using GNSS crosslink ranging observations</title><author>Meng, Yinan ; Fan, Shiwei ; Li, Gang ; Gao, Weiguang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-p136t-6c18a40518fdff71630c3894d32b3512e86bf4c844a9bb7c5eb1d3ba15c2d14b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>chi ; eng</language><creationdate>2014</creationdate><topic>Argon oxygen decarburizing</topic><topic>Autonomous</topic><topic>Crosslinking</topic><topic>Earth orbital environments</topic><topic>GNSS</topic><topic>Orbit determination</topic><topic>Satellite tracking</topic><topic>Satellites</topic><toplevel>online_resources</toplevel><creatorcontrib>Meng, Yinan</creatorcontrib><creatorcontrib>Fan, Shiwei</creatorcontrib><creatorcontrib>Li, Gang</creatorcontrib><creatorcontrib>Gao, Weiguang</creatorcontrib><collection>Electronics &amp; Communications Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Geomatics and Information Science of Wuhan University</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Meng, Yinan</au><au>Fan, Shiwei</au><au>Li, Gang</au><au>Gao, Weiguang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Orbit determination of medium-high earth orbital satellite using GNSS crosslink ranging observations</atitle><jtitle>Geomatics and Information Science of Wuhan University</jtitle><date>2014-04-01</date><risdate>2014</risdate><volume>39</volume><issue>4</issue><spage>445</spage><epage>449</epage><pages>445-449</pages><issn>1671-8860</issn><abstract>Precise orbit determination of medium and high earth orbital satellites mainly depends on ground-based tracking systems, which have limitations such as insufficient tracking arc, low accuracy, and are often unable to support autonomous navigation. The foundation of a GNSS crosslink network provides a new resolution for orbit determination of medium and high earth orbital satellites. This paper introduces a new method, used for orbit determination of medium and high earth orbital satellites based on GNSS crosslink ranging observations. The visibility, positioning accuracy, and crosslink budget has been analyzed and the simulative calculation of Autonomous Orbit Determination (AOD) was performed. The results show that with sufficient visible satellite numbers, positioning accuracy, and link margins, the AOD of medium-high earth orbital satellites using GNSS crosslink ranging observations can achieve a positioning error within 6 m in radial, 2 m along and across; the new method is feasible and can open new directions in the application of GNSS.</abstract><doi>10.13203/j.whugis20120215</doi><tpages>5</tpages></addata></record>
fulltext fulltext
identifier ISSN: 1671-8860
ispartof Geomatics and Information Science of Wuhan University, 2014-04, Vol.39 (4), p.445-449
issn 1671-8860
language chi ; eng
recordid cdi_proquest_miscellaneous_1701104843
source Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals
subjects Argon oxygen decarburizing
Autonomous
Crosslinking
Earth orbital environments
GNSS
Orbit determination
Satellite tracking
Satellites
title Orbit determination of medium-high earth orbital satellite using GNSS crosslink ranging observations
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-20T08%3A48%3A56IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Orbit%20determination%20of%20medium-high%20earth%20orbital%20satellite%20using%20GNSS%20crosslink%20ranging%20observations&rft.jtitle=Geomatics%20and%20Information%20Science%20of%20Wuhan%20University&rft.au=Meng,%20Yinan&rft.date=2014-04-01&rft.volume=39&rft.issue=4&rft.spage=445&rft.epage=449&rft.pages=445-449&rft.issn=1671-8860&rft_id=info:doi/10.13203/j.whugis20120215&rft_dat=%3Cproquest%3E1541418821%3C/proquest%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1541418821&rft_id=info:pmid/&rfr_iscdi=true