Loading…

Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system

The heading accuracy of an existing shipborne inertial navigation system (INS) is affected by the oscillatory heading error caused by the misalignment angles between the gyro case and gyro axes. The accuracy of the heading determination system (HDS), which consists of two quadruple GPS antenna array...

Full description

Saved in:
Bibliographic Details
Published in:GPS solutions 2017-07, Vol.21 (3), p.1059-1068
Main Authors: Hu, Peida, Huang, Chunan
Format: Article
Language:English
Subjects:
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by cdi_FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903
cites cdi_FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903
container_end_page 1068
container_issue 3
container_start_page 1059
container_title GPS solutions
container_volume 21
creator Hu, Peida
Huang, Chunan
description The heading accuracy of an existing shipborne inertial navigation system (INS) is affected by the oscillatory heading error caused by the misalignment angles between the gyro case and gyro axes. The accuracy of the heading determination system (HDS), which consists of two quadruple GPS antenna arrays, an INS, a total station surveying apparatus (TSSA), and two vessels, is affected by jump errors because of the degradation of tracking performance of the TSSA servo system in high dynamic conditions. Given that only pitch and roll of the INS are utilized in the HDS, we propose a high-accuracy heading determination system that combines the heading rate of the INS and linear fit of the heading difference between INS and HDS, to compensate for jump errors of HDS and oscillatory heading error of the INS. With the designed equipment, both jump errors and the oscillatory heading error can be suppressed effectively. The standard deviations of the heading errors are reduced from ±6 to ±2 and from ±8 to ±5 arcsec in mooring and sea tests, respectively, and a high accuracy of shipborne heading determination can be achieved since the oscillatory heading error is reduced to the 1 arcsec level.
doi_str_mv 10.1007/s10291-016-0590-5
format article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2259275495</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2259275495</sourcerecordid><originalsourceid>FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903</originalsourceid><addsrcrecordid>eNp1kMFKxDAQhoMouK4-gLeC5-hM26TJURZdhUWF1XNI0-m2i23XpD3s29tSwdOeZpj5vxn4GLtFuEeA7CEgxBo5oOQgNHBxxhYoYuSolDwfe1DjMMngkl2FsAeIQet0wfbbqj7knW8pqupdxa1zg7fuGFVki7rdRQX15Ju6tX3dtVFDfdUV0RCm1evblke2LaL1x5bnNlBxggrH0FNzzS5K-x3o5q8u2dfz0-fqhW_e16-rxw13Ccqep6VWNpepQp3kUCgpMRMFSExL5XIspUZEJUlmoJ1OqBQWkpKcs0S60JAs2d189-C7n4FCb_bd4NvxpYljoeNMpFqMKZxTzncheCrNwdeN9UeDYCalZlZqRqVmUmomJp6ZMGbbHfn_y6ehX49QeaM</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2259275495</pqid></control><display><type>article</type><title>Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system</title><source>Springer Nature</source><creator>Hu, Peida ; Huang, Chunan</creator><creatorcontrib>Hu, Peida ; Huang, Chunan</creatorcontrib><description>The heading accuracy of an existing shipborne inertial navigation system (INS) is affected by the oscillatory heading error caused by the misalignment angles between the gyro case and gyro axes. The accuracy of the heading determination system (HDS), which consists of two quadruple GPS antenna arrays, an INS, a total station surveying apparatus (TSSA), and two vessels, is affected by jump errors because of the degradation of tracking performance of the TSSA servo system in high dynamic conditions. Given that only pitch and roll of the INS are utilized in the HDS, we propose a high-accuracy heading determination system that combines the heading rate of the INS and linear fit of the heading difference between INS and HDS, to compensate for jump errors of HDS and oscillatory heading error of the INS. With the designed equipment, both jump errors and the oscillatory heading error can be suppressed effectively. The standard deviations of the heading errors are reduced from ±6 to ±2 and from ±8 to ±5 arcsec in mooring and sea tests, respectively, and a high accuracy of shipborne heading determination can be achieved since the oscillatory heading error is reduced to the 1 arcsec level.</description><identifier>ISSN: 1080-5370</identifier><identifier>EISSN: 1521-1886</identifier><identifier>DOI: 10.1007/s10291-016-0590-5</identifier><language>eng</language><publisher>Berlin/Heidelberg: Springer Berlin Heidelberg</publisher><subject>Accuracy ; Antenna arrays ; Atmospheric Sciences ; Automotive Engineering ; Earth and Environmental Science ; Earth Sciences ; Electrical Engineering ; Error reduction ; Geophysics/Geodesy ; Global positioning systems ; GPS ; Inertial navigation ; Misalignment ; Navigation systems ; Original Article ; Pitch (inclination) ; Rolling motion ; Satellite navigation systems ; Space Exploration and Astronautics ; Space Sciences (including Extraterrestrial Physics ; Surveying</subject><ispartof>GPS solutions, 2017-07, Vol.21 (3), p.1059-1068</ispartof><rights>Springer-Verlag Berlin Heidelberg 2016</rights><rights>GPS Solutions is a copyright of Springer, (2016). All Rights Reserved.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903</citedby><cites>FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903</cites><orcidid>0000-0003-4463-2221</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Hu, Peida</creatorcontrib><creatorcontrib>Huang, Chunan</creatorcontrib><title>Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system</title><title>GPS solutions</title><addtitle>GPS Solut</addtitle><description>The heading accuracy of an existing shipborne inertial navigation system (INS) is affected by the oscillatory heading error caused by the misalignment angles between the gyro case and gyro axes. The accuracy of the heading determination system (HDS), which consists of two quadruple GPS antenna arrays, an INS, a total station surveying apparatus (TSSA), and two vessels, is affected by jump errors because of the degradation of tracking performance of the TSSA servo system in high dynamic conditions. Given that only pitch and roll of the INS are utilized in the HDS, we propose a high-accuracy heading determination system that combines the heading rate of the INS and linear fit of the heading difference between INS and HDS, to compensate for jump errors of HDS and oscillatory heading error of the INS. With the designed equipment, both jump errors and the oscillatory heading error can be suppressed effectively. The standard deviations of the heading errors are reduced from ±6 to ±2 and from ±8 to ±5 arcsec in mooring and sea tests, respectively, and a high accuracy of shipborne heading determination can be achieved since the oscillatory heading error is reduced to the 1 arcsec level.</description><subject>Accuracy</subject><subject>Antenna arrays</subject><subject>Atmospheric Sciences</subject><subject>Automotive Engineering</subject><subject>Earth and Environmental Science</subject><subject>Earth Sciences</subject><subject>Electrical Engineering</subject><subject>Error reduction</subject><subject>Geophysics/Geodesy</subject><subject>Global positioning systems</subject><subject>GPS</subject><subject>Inertial navigation</subject><subject>Misalignment</subject><subject>Navigation systems</subject><subject>Original Article</subject><subject>Pitch (inclination)</subject><subject>Rolling motion</subject><subject>Satellite navigation systems</subject><subject>Space Exploration and Astronautics</subject><subject>Space Sciences (including Extraterrestrial Physics</subject><subject>Surveying</subject><issn>1080-5370</issn><issn>1521-1886</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp1kMFKxDAQhoMouK4-gLeC5-hM26TJURZdhUWF1XNI0-m2i23XpD3s29tSwdOeZpj5vxn4GLtFuEeA7CEgxBo5oOQgNHBxxhYoYuSolDwfe1DjMMngkl2FsAeIQet0wfbbqj7knW8pqupdxa1zg7fuGFVki7rdRQX15Ju6tX3dtVFDfdUV0RCm1evblke2LaL1x5bnNlBxggrH0FNzzS5K-x3o5q8u2dfz0-fqhW_e16-rxw13Ccqep6VWNpepQp3kUCgpMRMFSExL5XIspUZEJUlmoJ1OqBQWkpKcs0S60JAs2d189-C7n4FCb_bd4NvxpYljoeNMpFqMKZxTzncheCrNwdeN9UeDYCalZlZqRqVmUmomJp6ZMGbbHfn_y6ehX49QeaM</recordid><startdate>20170701</startdate><enddate>20170701</enddate><creator>Hu, Peida</creator><creator>Huang, Chunan</creator><general>Springer Berlin Heidelberg</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BHPHI</scope><scope>BKSAR</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>PCBAR</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><orcidid>https://orcid.org/0000-0003-4463-2221</orcidid></search><sort><creationdate>20170701</creationdate><title>Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system</title><author>Hu, Peida ; Huang, Chunan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Accuracy</topic><topic>Antenna arrays</topic><topic>Atmospheric Sciences</topic><topic>Automotive Engineering</topic><topic>Earth and Environmental Science</topic><topic>Earth Sciences</topic><topic>Electrical Engineering</topic><topic>Error reduction</topic><topic>Geophysics/Geodesy</topic><topic>Global positioning systems</topic><topic>GPS</topic><topic>Inertial navigation</topic><topic>Misalignment</topic><topic>Navigation systems</topic><topic>Original Article</topic><topic>Pitch (inclination)</topic><topic>Rolling motion</topic><topic>Satellite navigation systems</topic><topic>Space Exploration and Astronautics</topic><topic>Space Sciences (including Extraterrestrial Physics</topic><topic>Surveying</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hu, Peida</creatorcontrib><creatorcontrib>Huang, Chunan</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>ProQuest Central</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Natural Science Collection</collection><collection>Earth, Atmospheric &amp; Aquatic Science Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Earth, Atmospheric &amp; Aquatic Science Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><jtitle>GPS solutions</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hu, Peida</au><au>Huang, Chunan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system</atitle><jtitle>GPS solutions</jtitle><stitle>GPS Solut</stitle><date>2017-07-01</date><risdate>2017</risdate><volume>21</volume><issue>3</issue><spage>1059</spage><epage>1068</epage><pages>1059-1068</pages><issn>1080-5370</issn><eissn>1521-1886</eissn><abstract>The heading accuracy of an existing shipborne inertial navigation system (INS) is affected by the oscillatory heading error caused by the misalignment angles between the gyro case and gyro axes. The accuracy of the heading determination system (HDS), which consists of two quadruple GPS antenna arrays, an INS, a total station surveying apparatus (TSSA), and two vessels, is affected by jump errors because of the degradation of tracking performance of the TSSA servo system in high dynamic conditions. Given that only pitch and roll of the INS are utilized in the HDS, we propose a high-accuracy heading determination system that combines the heading rate of the INS and linear fit of the heading difference between INS and HDS, to compensate for jump errors of HDS and oscillatory heading error of the INS. With the designed equipment, both jump errors and the oscillatory heading error can be suppressed effectively. The standard deviations of the heading errors are reduced from ±6 to ±2 and from ±8 to ±5 arcsec in mooring and sea tests, respectively, and a high accuracy of shipborne heading determination can be achieved since the oscillatory heading error is reduced to the 1 arcsec level.</abstract><cop>Berlin/Heidelberg</cop><pub>Springer Berlin Heidelberg</pub><doi>10.1007/s10291-016-0590-5</doi><tpages>10</tpages><orcidid>https://orcid.org/0000-0003-4463-2221</orcidid></addata></record>
fulltext fulltext
identifier ISSN: 1080-5370
ispartof GPS solutions, 2017-07, Vol.21 (3), p.1059-1068
issn 1080-5370
1521-1886
language eng
recordid cdi_proquest_journals_2259275495
source Springer Nature
subjects Accuracy
Antenna arrays
Atmospheric Sciences
Automotive Engineering
Earth and Environmental Science
Earth Sciences
Electrical Engineering
Error reduction
Geophysics/Geodesy
Global positioning systems
GPS
Inertial navigation
Misalignment
Navigation systems
Original Article
Pitch (inclination)
Rolling motion
Satellite navigation systems
Space Exploration and Astronautics
Space Sciences (including Extraterrestrial Physics
Surveying
title Shipborne high-accuracy heading determination method using INS- and GPS-based heading determination system
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T19%3A03%3A41IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Shipborne%20high-accuracy%20heading%20determination%20method%20using%20INS-%20and%20GPS-based%20heading%20determination%20system&rft.jtitle=GPS%20solutions&rft.au=Hu,%20Peida&rft.date=2017-07-01&rft.volume=21&rft.issue=3&rft.spage=1059&rft.epage=1068&rft.pages=1059-1068&rft.issn=1080-5370&rft.eissn=1521-1886&rft_id=info:doi/10.1007/s10291-016-0590-5&rft_dat=%3Cproquest_cross%3E2259275495%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c316t-4f98ab648193b0d866175d0614f8cb1f6911186e6709c93ef5a03feccaee9d903%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2259275495&rft_id=info:pmid/&rfr_iscdi=true