Loading…

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...

Full description

Saved in:
Bibliographic Details
Published in:IEEE transactions on aerospace and electronic systems 1998-01, Vol.34 (1), p.338-340
Main Authors: Markley, F.L., Bar-Itzhack, I.Y.
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-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3
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
fullrecord <record><control><sourceid>proquest_ieee_</sourceid><recordid>TN_cdi_proquest_miscellaneous_26659185</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>640293</ieee_id><sourcerecordid>28954732</sourcerecordid><originalsourceid>FETCH-LOGICAL-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3</originalsourceid><addsrcrecordid>eNqNkEtLxDAUhYMoWEfBtauuRJCOuc2rWcrgCwbcOOuQ5gGVtqlJB_TfG-ngVleHw_24HD6ELgGvAbC8E2tOcS3JESqAMVFJjskxKjCGppI1g1N0ltJ7rrShpEC3u9GEMc1Rd6OzZZjmbtB9mfuYfIiDnrswljli93mOTrzuk7s45ArtHh_eNs_V9vXpZXO_rQwRMFfMGNBWW7DGi7bhmrW4dVjnUYywllumHSUW8jzPrcVei5py7rnTQC1pyQpdL3-nGD72Ls1q6JJxfa9HF_ZJ1Y1kVJD6HyDFBID-DXLOJDQsgzcLaGJIKTqvppiFxC8FWP34VUItfjN6taCdc-4XOxy_AYqMdSo</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>26659185</pqid></control><display><type>article</type><title>Unconstrained optimal transformation matrix</title><source>IEEE Electronic Library (IEL) Journals</source><creator>Markley, F.L. ; Bar-Itzhack, I.Y.</creator><creatorcontrib>Markley, F.L. ; Bar-Itzhack, I.Y.</creatorcontrib><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.</description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/7.640293</identifier><identifier>CODEN: IEARAX</identifier><language>eng</language><publisher>IEEE</publisher><subject>Constraint optimization ; Loss measurement ; Protection ; Quaternions ; Satellites ; Space vehicles ; Symmetric matrices ; US Government ; Weight measurement</subject><ispartof>IEEE transactions on aerospace and electronic systems, 1998-01, Vol.34 (1), p.338-340</ispartof><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3</citedby><cites>FETCH-LOGICAL-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/640293$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,54796</link.rule.ids></links><search><creatorcontrib>Markley, F.L.</creatorcontrib><creatorcontrib>Bar-Itzhack, I.Y.</creatorcontrib><title>Unconstrained optimal transformation matrix</title><title>IEEE transactions on aerospace and electronic systems</title><addtitle>T-AES</addtitle><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.</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 &amp; Communications Abstracts</collection><collection>Mechanical &amp; 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>
fulltext fulltext
identifier ISSN: 0018-9251
ispartof IEEE transactions on aerospace and electronic systems, 1998-01, Vol.34 (1), p.338-340
issn 0018-9251
1557-9603
language eng
recordid cdi_proquest_miscellaneous_26659185
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
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-02T21%3A50%3A42IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_ieee_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Unconstrained%20optimal%20transformation%20matrix&rft.jtitle=IEEE%20transactions%20on%20aerospace%20and%20electronic%20systems&rft.au=Markley,%20F.L.&rft.date=1998-01&rft.volume=34&rft.issue=1&rft.spage=338&rft.epage=340&rft.pages=338-340&rft.issn=0018-9251&rft.eissn=1557-9603&rft.coden=IEARAX&rft_id=info:doi/10.1109/7.640293&rft_dat=%3Cproquest_ieee_%3E28954732%3C/proquest_ieee_%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c371t-5cc1adad1dcf7b86a5b0be0a293535b6d5ae43d1155f6dd0fa72466f6ea14d3b3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=26659185&rft_id=info:pmid/&rft_ieee_id=640293&rfr_iscdi=true