Attitude sensors relative angular misalignment estimation in integrated navigation systems

When using modern navigation systems as part of an on-board system, the navigation task can be solved in several ways: using positional, velocity and angular corrections, and systems using measurements of various physical nature—radio, such as short-range and long-range navigation radio systems, GLO...

Full description

Saved in:
Bibliographic Details
Published in:MATEC web of conferences 2022, Vol.362, p.1015
Main Authors: Kuznetsov, Ivan, Veremeenko, Konstantin, Zharkov, Maksim, Pronkin, Andrey
Format: Article
Language:English
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-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033
cites cdi_FETCH-LOGICAL-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033
container_end_page
container_issue
container_start_page 1015
container_title MATEC web of conferences
container_volume 362
creator Kuznetsov, Ivan
Veremeenko, Konstantin
Zharkov, Maksim
Pronkin, Andrey
description When using modern navigation systems as part of an on-board system, the navigation task can be solved in several ways: using positional, velocity and angular corrections, and systems using measurements of various physical nature—radio, such as short-range and long-range navigation radio systems, GLONASS/GPS satellite global navigation systems, optical—celestial navigation systems—can operate as correctors. The best performance of INS and its sensors (gyroscopes and accelerometers) errors estimation can be obtained when all types of correction are implemented simultaneously. At the same time, it is particularly difficult to implement correction according to attitude parameters due to the fact that the measuring axes of the INS and correctors may not match on board of moving objects. Such a mismatch is commonly called relative angular misalignment. The paper considers a possible approach to the attitude sensors relative angular misalignment estimation in integrated navigation systems (NS), carried out in motion when the NS is in operating mode.
doi_str_mv 10.1051/matecconf/202236201015
format article
fullrecord <record><control><sourceid>doaj_cross</sourceid><recordid>TN_cdi_doaj_primary_oai_doaj_org_article_2cf531323111413ca1e7c692f449206b</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><doaj_id>oai_doaj_org_article_2cf531323111413ca1e7c692f449206b</doaj_id><sourcerecordid>oai_doaj_org_article_2cf531323111413ca1e7c692f449206b</sourcerecordid><originalsourceid>FETCH-LOGICAL-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033</originalsourceid><addsrcrecordid>eNpNkNtqwzAQREVpoSHNLxT_gJtdSZasxxB6CQT60kLpi5Bl2Sj4UiQlkL-v05QQWNhlBs4OQ8gjwhNCgcveJGftODRLCpQyQQEBixsyo1RgPglft1f3PVnEuAMAZEqCkjPyvUrJp33tsuiGOIaYBdeZ5A8uM0O770zIeh9N59uhd0PKXEx--unHIfOnSa4NU4Q6G8zBt2cjHmNyfXwgd43polv87zn5fHn-WL_l2_fXzXq1zS1FXuRSGpS1BCgptxapKhQvuayswJrWvCosVEoZBgUVpShNU9SSg-DCYVVTYGxONmduPZqd_glTvnDUo_H6TxhDq01I3nZOU9sUDBlliMiRWYNOWqFow7miIKqJJc4sG8YYg2suPAR9KlxfCtfXhbNfbOF2iw</addsrcrecordid><sourcetype>Open Website</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Attitude sensors relative angular misalignment estimation in integrated navigation systems</title><source>Publicly Available Content Database (Proquest) (PQ_SDU_P3)</source><creator>Kuznetsov, Ivan ; Veremeenko, Konstantin ; Zharkov, Maksim ; Pronkin, Andrey</creator><contributor>Mikilyan, M. ; Severina, N.S.</contributor><creatorcontrib>Kuznetsov, Ivan ; Veremeenko, Konstantin ; Zharkov, Maksim ; Pronkin, Andrey ; Mikilyan, M. ; Severina, N.S.</creatorcontrib><description>When using modern navigation systems as part of an on-board system, the navigation task can be solved in several ways: using positional, velocity and angular corrections, and systems using measurements of various physical nature—radio, such as short-range and long-range navigation radio systems, GLONASS/GPS satellite global navigation systems, optical—celestial navigation systems—can operate as correctors. The best performance of INS and its sensors (gyroscopes and accelerometers) errors estimation can be obtained when all types of correction are implemented simultaneously. At the same time, it is particularly difficult to implement correction according to attitude parameters due to the fact that the measuring axes of the INS and correctors may not match on board of moving objects. Such a mismatch is commonly called relative angular misalignment. The paper considers a possible approach to the attitude sensors relative angular misalignment estimation in integrated navigation systems (NS), carried out in motion when the NS is in operating mode.</description><identifier>ISSN: 2261-236X</identifier><identifier>EISSN: 2261-236X</identifier><identifier>DOI: 10.1051/matecconf/202236201015</identifier><language>eng</language><publisher>EDP Sciences</publisher><ispartof>MATEC web of conferences, 2022, Vol.362, p.1015</ispartof><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033</citedby><cites>FETCH-LOGICAL-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,4024,27923,27924,27925</link.rule.ids></links><search><contributor>Mikilyan, M.</contributor><contributor>Severina, N.S.</contributor><creatorcontrib>Kuznetsov, Ivan</creatorcontrib><creatorcontrib>Veremeenko, Konstantin</creatorcontrib><creatorcontrib>Zharkov, Maksim</creatorcontrib><creatorcontrib>Pronkin, Andrey</creatorcontrib><title>Attitude sensors relative angular misalignment estimation in integrated navigation systems</title><title>MATEC web of conferences</title><description>When using modern navigation systems as part of an on-board system, the navigation task can be solved in several ways: using positional, velocity and angular corrections, and systems using measurements of various physical nature—radio, such as short-range and long-range navigation radio systems, GLONASS/GPS satellite global navigation systems, optical—celestial navigation systems—can operate as correctors. The best performance of INS and its sensors (gyroscopes and accelerometers) errors estimation can be obtained when all types of correction are implemented simultaneously. At the same time, it is particularly difficult to implement correction according to attitude parameters due to the fact that the measuring axes of the INS and correctors may not match on board of moving objects. Such a mismatch is commonly called relative angular misalignment. The paper considers a possible approach to the attitude sensors relative angular misalignment estimation in integrated navigation systems (NS), carried out in motion when the NS is in operating mode.</description><issn>2261-236X</issn><issn>2261-236X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><sourceid>DOA</sourceid><recordid>eNpNkNtqwzAQREVpoSHNLxT_gJtdSZasxxB6CQT60kLpi5Bl2Sj4UiQlkL-v05QQWNhlBs4OQ8gjwhNCgcveJGftODRLCpQyQQEBixsyo1RgPglft1f3PVnEuAMAZEqCkjPyvUrJp33tsuiGOIaYBdeZ5A8uM0O770zIeh9N59uhd0PKXEx--unHIfOnSa4NU4Q6G8zBt2cjHmNyfXwgd43polv87zn5fHn-WL_l2_fXzXq1zS1FXuRSGpS1BCgptxapKhQvuayswJrWvCosVEoZBgUVpShNU9SSg-DCYVVTYGxONmduPZqd_glTvnDUo_H6TxhDq01I3nZOU9sUDBlliMiRWYNOWqFow7miIKqJJc4sG8YYg2suPAR9KlxfCtfXhbNfbOF2iw</recordid><startdate>2022</startdate><enddate>2022</enddate><creator>Kuznetsov, Ivan</creator><creator>Veremeenko, Konstantin</creator><creator>Zharkov, Maksim</creator><creator>Pronkin, Andrey</creator><general>EDP Sciences</general><scope>AAYXX</scope><scope>CITATION</scope><scope>DOA</scope></search><sort><creationdate>2022</creationdate><title>Attitude sensors relative angular misalignment estimation in integrated navigation systems</title><author>Kuznetsov, Ivan ; Veremeenko, Konstantin ; Zharkov, Maksim ; Pronkin, Andrey</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kuznetsov, Ivan</creatorcontrib><creatorcontrib>Veremeenko, Konstantin</creatorcontrib><creatorcontrib>Zharkov, Maksim</creatorcontrib><creatorcontrib>Pronkin, Andrey</creatorcontrib><collection>CrossRef</collection><collection>DOAJ Directory of Open Access Journals</collection><jtitle>MATEC web of conferences</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kuznetsov, Ivan</au><au>Veremeenko, Konstantin</au><au>Zharkov, Maksim</au><au>Pronkin, Andrey</au><au>Mikilyan, M.</au><au>Severina, N.S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Attitude sensors relative angular misalignment estimation in integrated navigation systems</atitle><jtitle>MATEC web of conferences</jtitle><date>2022</date><risdate>2022</risdate><volume>362</volume><spage>1015</spage><pages>1015-</pages><issn>2261-236X</issn><eissn>2261-236X</eissn><abstract>When using modern navigation systems as part of an on-board system, the navigation task can be solved in several ways: using positional, velocity and angular corrections, and systems using measurements of various physical nature—radio, such as short-range and long-range navigation radio systems, GLONASS/GPS satellite global navigation systems, optical—celestial navigation systems—can operate as correctors. The best performance of INS and its sensors (gyroscopes and accelerometers) errors estimation can be obtained when all types of correction are implemented simultaneously. At the same time, it is particularly difficult to implement correction according to attitude parameters due to the fact that the measuring axes of the INS and correctors may not match on board of moving objects. Such a mismatch is commonly called relative angular misalignment. The paper considers a possible approach to the attitude sensors relative angular misalignment estimation in integrated navigation systems (NS), carried out in motion when the NS is in operating mode.</abstract><pub>EDP Sciences</pub><doi>10.1051/matecconf/202236201015</doi><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 2261-236X
ispartof MATEC web of conferences, 2022, Vol.362, p.1015
issn 2261-236X
2261-236X
language eng
recordid cdi_doaj_primary_oai_doaj_org_article_2cf531323111413ca1e7c692f449206b
source Publicly Available Content Database (Proquest) (PQ_SDU_P3)
title Attitude sensors relative angular misalignment estimation in integrated navigation systems
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T07%3A16%3A58IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-doaj_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Attitude%20sensors%20relative%20angular%20misalignment%20estimation%20in%20integrated%20navigation%20systems&rft.jtitle=MATEC%20web%20of%20conferences&rft.au=Kuznetsov,%20Ivan&rft.date=2022&rft.volume=362&rft.spage=1015&rft.pages=1015-&rft.issn=2261-236X&rft.eissn=2261-236X&rft_id=info:doi/10.1051/matecconf/202236201015&rft_dat=%3Cdoaj_cross%3Eoai_doaj_org_article_2cf531323111413ca1e7c692f449206b%3C/doaj_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c2145-77a17d700824cc129594847bc61d2d4b5c0b99a30526868af5d740646e1bd2033%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true