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...
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Veröffentlicht in: | Geomatics and Information Science of Wuhan University 2014-04, Vol.39 (4), p.445-449 |
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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 |
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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 & 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> |
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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 |
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