Research on initial alignment method of vehicle-mounted SINS based on reverse navigation
In order to improve the alignment accuracy and speed of vehicle-mounted SINS, an initial alignment scheme of “inertial solidification alignment + Kalman filter fine alignment based on reverse navigation” is proposed in this paper. Firstly, an inertial solidification alignment algorithm is derived, t...
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Veröffentlicht in: | Journal of physics. Conference series 2021-03, Vol.1846 (1), p.12075 |
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description | In order to improve the alignment accuracy and speed of vehicle-mounted SINS, an initial alignment scheme of “inertial solidification alignment + Kalman filter fine alignment based on reverse navigation” is proposed in this paper. Firstly, an inertial solidification alignment algorithm is derived, the initial alignment problem is transformed into Wahba problem, and the optimal attitude matrix at the initial moment is obtained by singular value decomposition algorithm. The inertial solidification alignment algorithm is more concise and intuitive than the traditional alignment algorithm of geocentric inertial coordinate system. Then, we analyzed the effectiveness of rotation modulation technology to improve alignment accuracy theoretically and proved it by simulation. And it is pointed out that the application platform space is limited and the system cost is increased when using this technology. Furthermore, in order to overcome the shortcomings of using rotation modulation technology, a Kalman filter algorithm based on reverse navigation is derived. By reusing the data stored during the inertial solidification alignment, the alignment time is extended equivalently, the initial attitude error is reduced and the attitude calculation accuracy after forward navigation is improved, higher precision alignment is realized. Finally, the effectiveness of the initial alignment scheme is verified by simulation. |
doi_str_mv | 10.1088/1742-6596/1846/1/012075 |
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Firstly, an inertial solidification alignment algorithm is derived, the initial alignment problem is transformed into Wahba problem, and the optimal attitude matrix at the initial moment is obtained by singular value decomposition algorithm. The inertial solidification alignment algorithm is more concise and intuitive than the traditional alignment algorithm of geocentric inertial coordinate system. Then, we analyzed the effectiveness of rotation modulation technology to improve alignment accuracy theoretically and proved it by simulation. And it is pointed out that the application platform space is limited and the system cost is increased when using this technology. Furthermore, in order to overcome the shortcomings of using rotation modulation technology, a Kalman filter algorithm based on reverse navigation is derived. By reusing the data stored during the inertial solidification alignment, the alignment time is extended equivalently, the initial attitude error is reduced and the attitude calculation accuracy after forward navigation is improved, higher precision alignment is realized. Finally, the effectiveness of the initial alignment scheme is verified by simulation.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/1846/1/012075</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Accuracy ; Algorithms ; Alignment ; Attitudes ; Error reduction ; Inertial coordinates ; Kalman filters ; Modulation ; Navigation ; Physics ; Rotation ; Singular value decomposition ; Solidification ; Technology utilization</subject><ispartof>Journal of physics. Conference series, 2021-03, Vol.1846 (1), p.12075</ispartof><rights>2021. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c2345-7aa809741577744175abe08bfbd98a8d4aa8ca7a397eecd6bdf5edc01552d8de3</cites></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>Yang, Chen</creatorcontrib><creatorcontrib>Cai, Yuanwen</creatorcontrib><creatorcontrib>Xin, Chaojun</creatorcontrib><creatorcontrib>Shi, Meiling</creatorcontrib><title>Research on initial alignment method of vehicle-mounted SINS based on reverse navigation</title><title>Journal of physics. Conference series</title><description>In order to improve the alignment accuracy and speed of vehicle-mounted SINS, an initial alignment scheme of “inertial solidification alignment + Kalman filter fine alignment based on reverse navigation” is proposed in this paper. Firstly, an inertial solidification alignment algorithm is derived, the initial alignment problem is transformed into Wahba problem, and the optimal attitude matrix at the initial moment is obtained by singular value decomposition algorithm. The inertial solidification alignment algorithm is more concise and intuitive than the traditional alignment algorithm of geocentric inertial coordinate system. Then, we analyzed the effectiveness of rotation modulation technology to improve alignment accuracy theoretically and proved it by simulation. And it is pointed out that the application platform space is limited and the system cost is increased when using this technology. Furthermore, in order to overcome the shortcomings of using rotation modulation technology, a Kalman filter algorithm based on reverse navigation is derived. By reusing the data stored during the inertial solidification alignment, the alignment time is extended equivalently, the initial attitude error is reduced and the attitude calculation accuracy after forward navigation is improved, higher precision alignment is realized. Finally, the effectiveness of the initial alignment scheme is verified by simulation.</description><subject>Accuracy</subject><subject>Algorithms</subject><subject>Alignment</subject><subject>Attitudes</subject><subject>Error reduction</subject><subject>Inertial coordinates</subject><subject>Kalman filters</subject><subject>Modulation</subject><subject>Navigation</subject><subject>Physics</subject><subject>Rotation</subject><subject>Singular value decomposition</subject><subject>Solidification</subject><subject>Technology utilization</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>ABUWG</sourceid><sourceid>AFKRA</sourceid><sourceid>AZQEC</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNo9kN1KAzEQhYMoWKvPYMDrtclu0mQvpfhTEAWr4F3IJrNtym5Sk23BtzdLpXMxc-CcmYEPoVtK7imRckYFK4s5r-czKlluM0JLIvgZmpyc85OW8hJdpbQlpMolJuj7AxLoaDY4eOy8G5zusO7c2vfgB9zDsAkWhxYfYONMB0Uf9n4Ai1fLtxVudMoyb0Y4QEyAvT64tR5c8NfootVdgpv_OUVfT4-fi5fi9f15uXh4LUxZMV4IrSWpBaNcCMEYFVw3QGTTNraWWlqWfaOFrmoBYOy8sS0HawjlvLTSQjVFd8e7uxh-9pAGtQ376PNLVXJa1lRQynJKHFMmhpQitGoXXa_jr6JEjRjVCEiNsNSIUVF1xFj9AbIeZnU</recordid><startdate>20210301</startdate><enddate>20210301</enddate><creator>Yang, Chen</creator><creator>Cai, Yuanwen</creator><creator>Xin, Chaojun</creator><creator>Shi, Meiling</creator><general>IOP Publishing</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20210301</creationdate><title>Research on initial alignment method of vehicle-mounted SINS based on reverse navigation</title><author>Yang, Chen ; Cai, Yuanwen ; Xin, Chaojun ; Shi, Meiling</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c2345-7aa809741577744175abe08bfbd98a8d4aa8ca7a397eecd6bdf5edc01552d8de3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Accuracy</topic><topic>Algorithms</topic><topic>Alignment</topic><topic>Attitudes</topic><topic>Error reduction</topic><topic>Inertial coordinates</topic><topic>Kalman filters</topic><topic>Modulation</topic><topic>Navigation</topic><topic>Physics</topic><topic>Rotation</topic><topic>Singular value decomposition</topic><topic>Solidification</topic><topic>Technology utilization</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yang, Chen</creatorcontrib><creatorcontrib>Cai, Yuanwen</creatorcontrib><creatorcontrib>Xin, Chaojun</creatorcontrib><creatorcontrib>Shi, Meiling</creatorcontrib><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni Edition)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Collection</collection><collection>ProQuest Central Essentials</collection><collection>ProQuest Central</collection><collection>Technology 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>Advanced Technologies & Aerospace Database</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Journal of physics. Conference series</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yang, Chen</au><au>Cai, Yuanwen</au><au>Xin, Chaojun</au><au>Shi, Meiling</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Research on initial alignment method of vehicle-mounted SINS based on reverse navigation</atitle><jtitle>Journal of physics. Conference series</jtitle><date>2021-03-01</date><risdate>2021</risdate><volume>1846</volume><issue>1</issue><spage>12075</spage><pages>12075-</pages><issn>1742-6588</issn><eissn>1742-6596</eissn><abstract>In order to improve the alignment accuracy and speed of vehicle-mounted SINS, an initial alignment scheme of “inertial solidification alignment + Kalman filter fine alignment based on reverse navigation” is proposed in this paper. Firstly, an inertial solidification alignment algorithm is derived, the initial alignment problem is transformed into Wahba problem, and the optimal attitude matrix at the initial moment is obtained by singular value decomposition algorithm. The inertial solidification alignment algorithm is more concise and intuitive than the traditional alignment algorithm of geocentric inertial coordinate system. Then, we analyzed the effectiveness of rotation modulation technology to improve alignment accuracy theoretically and proved it by simulation. And it is pointed out that the application platform space is limited and the system cost is increased when using this technology. Furthermore, in order to overcome the shortcomings of using rotation modulation technology, a Kalman filter algorithm based on reverse navigation is derived. By reusing the data stored during the inertial solidification alignment, the alignment time is extended equivalently, the initial attitude error is reduced and the attitude calculation accuracy after forward navigation is improved, higher precision alignment is realized. Finally, the effectiveness of the initial alignment scheme is verified by simulation.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1742-6596/1846/1/012075</doi><oa>free_for_read</oa></addata></record> |
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subjects | Accuracy Algorithms Alignment Attitudes Error reduction Inertial coordinates Kalman filters Modulation Navigation Physics Rotation Singular value decomposition Solidification Technology utilization |
title | Research on initial alignment method of vehicle-mounted SINS based on reverse navigation |
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