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Unconstrained optimal transformation matrix
We generalize Brock's minimization of the loss function proposed by Wahba to give a least-squares estimate of satellite attitude. We follow Brock in relaxing Wahba's requirement that the minimizing attitude matrix be orthogonal, and discuss the statistical properties of our new solution an...
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Published in: | IEEE transactions on aerospace and electronic systems 1998-01, Vol.34 (1), p.338-340 |
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cites | cdi_FETCH-LOGICAL-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3 |
container_end_page | 340 |
container_issue | 1 |
container_start_page | 338 |
container_title | IEEE transactions on aerospace and electronic systems |
container_volume | 34 |
creator | Markley, F.L. Bar-Itzhack, I.Y. |
description | We generalize Brock's minimization of the loss function proposed by Wahba to give a least-squares estimate of satellite attitude. We follow Brock in relaxing Wahba's requirement that the minimizing attitude matrix be orthogonal, and discuss the statistical properties of our new solution and its relation to existing attitude estimation algorithms. |
doi_str_mv | 10.1109/7.640293 |
format | article |
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We follow Brock in relaxing Wahba's requirement that the minimizing attitude matrix be orthogonal, and discuss the statistical properties of our new solution and its relation to existing attitude estimation algorithms.</description><subject>Constraint optimization</subject><subject>Loss measurement</subject><subject>Protection</subject><subject>Quaternions</subject><subject>Satellites</subject><subject>Space vehicles</subject><subject>Symmetric matrices</subject><subject>US Government</subject><subject>Weight measurement</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1998</creationdate><recordtype>article</recordtype><recordid>eNqNkEtLxDAUhYMoWEfBtauuRJCOuc2rWcrgCwbcOOuQ5gGVtqlJB_TfG-ngVleHw_24HD6ELgGvAbC8E2tOcS3JESqAMVFJjskxKjCGppI1g1N0ltJ7rrShpEC3u9GEMc1Rd6OzZZjmbtB9mfuYfIiDnrswljli93mOTrzuk7s45ArtHh_eNs_V9vXpZXO_rQwRMFfMGNBWW7DGi7bhmrW4dVjnUYywllumHSUW8jzPrcVei5py7rnTQC1pyQpdL3-nGD72Ls1q6JJxfa9HF_ZJ1Y1kVJD6HyDFBID-DXLOJDQsgzcLaGJIKTqvppiFxC8FWP34VUItfjN6taCdc-4XOxy_AYqMdSo</recordid><startdate>199801</startdate><enddate>199801</enddate><creator>Markley, F.L.</creator><creator>Bar-Itzhack, I.Y.</creator><general>IEEE</general><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope><scope>7SP</scope><scope>7TB</scope><scope>FR3</scope></search><sort><creationdate>199801</creationdate><title>Unconstrained optimal transformation matrix</title><author>Markley, F.L. ; Bar-Itzhack, I.Y.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1998</creationdate><topic>Constraint optimization</topic><topic>Loss measurement</topic><topic>Protection</topic><topic>Quaternions</topic><topic>Satellites</topic><topic>Space vehicles</topic><topic>Symmetric matrices</topic><topic>US Government</topic><topic>Weight measurement</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Markley, F.L.</creatorcontrib><creatorcontrib>Bar-Itzhack, I.Y.</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Xplore</collection><collection>CrossRef</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Engineering Research Database</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Markley, F.L.</au><au>Bar-Itzhack, I.Y.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Unconstrained optimal transformation matrix</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>1998-01</date><risdate>1998</risdate><volume>34</volume><issue>1</issue><spage>338</spage><epage>340</epage><pages>338-340</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>We generalize Brock's minimization of the loss function proposed by Wahba to give a least-squares estimate of satellite attitude. We follow Brock in relaxing Wahba's requirement that the minimizing attitude matrix be orthogonal, and discuss the statistical properties of our new solution and its relation to existing attitude estimation algorithms.</abstract><pub>IEEE</pub><doi>10.1109/7.640293</doi><tpages>3</tpages><oa>free_for_read</oa></addata></record> |
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ispartof | IEEE transactions on aerospace and electronic systems, 1998-01, Vol.34 (1), p.338-340 |
issn | 0018-9251 1557-9603 |
language | eng |
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source | IEEE Electronic Library (IEL) Journals |
subjects | Constraint optimization Loss measurement Protection Quaternions Satellites Space vehicles Symmetric matrices US Government Weight measurement |
title | Unconstrained optimal transformation matrix |
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