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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3LEC632
Repositorysid.inpe.br/mtc-m21b/2016/04.01.12.18
Last Update2016:04.01.12.19.58 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2016/04.01.12.18.09
Metadata Last Update2021:02.11.18.12.32 (UTC) administrator
DOI10.5028/jatm.v8i1.509
ISSN1984-9648
Labelself-archiving-INPE-MCTI-GOV-BR
Citation KeyGarciaKugaZana:2016:UnKaFi
TitleUnscented Kalman filter for determination of spacecraft attitude using different attitude parameterizations and real data
Year2016
Monthjan./mar.
Access Date2024, May 18
Type of Workjournal article
Secondary TypePRE PN
Number of Files1
Size820 KiB
2. Context
Author1 Garcia, Roberta Veloso
2 Kuga, Helio Koiti
3 Zanardi, Maria Cecília F. P. S.
Resume Identifier1
2 8JMKD3MGP5W/3C9JHC9
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Universidade de São Paulo (USP)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Federal do ABC (UFABC)
Author e-Mail Address1 robertagarcia@usp.br
2 helio.kuga@inpe.br
JournalJournal of Aerospace Technology and Management
Volume8
Number1
Pages82-90
Secondary MarkB2_PLANEJAMENTO_URBANO_E_REGIONAL_/_DEMOGRAFIA B3_INTERDISCIPLINAR B4_GEOCIÊNCIAS B4_ENGENHARIAS_II B4_CIÊNCIAS_AMBIENTAIS B5_ENGENHARIAS_IV B5_ENGENHARIAS_III B5_CIÊNCIA_DA_COMPUTAÇÃO C_ASTRONOMIA_/_FÍSICA
History (UTC)2016-04-01 12:18:09 :: simone -> administrator ::
2016-07-04 12:29:58 :: administrator -> simone :: 2016
2016-12-26 16:35:23 :: simone -> administrator :: 2016
2021-02-11 18:12:32 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAttitude estimation
Real data
Unscented Kalman Filter
Extended Kalman Filter
Quaternion
Euler angles
AbstractThe non-linear estimators are certainly the most important algorithms applied to real problems, especially those involving the attitude estimation of spacecraft. The purpose of this paper was to use real data of sensors to analyze the behavior of Unscented Kalman Filter (UKF) in attitude estimation problems when it is represented in different ways and compare it with the standard estimator for non-linear estimation problems. The robustness of the estimation was performed when this was subjected to imprecise initial conditions. The attitude parametrization was described in Euler angles, quaternion and quaternion incremental. The satellite China-Brazil Earth Resources Satellite and measurements provided by the Satellite Control Center of the Instituto Nacional de Pesquisas Espaciais were considered in the study. The results indicate that the behaviors for both estimators were equivalent for such parameterizations under the same conditions. However, comparing the Unscented Kalman Filter with the standard filter for non-linear systems, Extended Kalman Filter (EKF), it was observed that, in the presence of inaccurate initial conditions, the Unscented Kalman Filter presented a fast convergence whereas Extended Kalman Filter had problems and only converged later on.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Unscented Kalman filter...
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4. Conditions of access and use
data URLhttp://mtc-m21b.sid.inpe.br/ibi/8JMKD3MGP3W34P/3LEC632
zipped data URLhttp://mtc-m21b.sid.inpe.br/zip/8JMKD3MGP3W34P/3LEC632
Languageen
Target Filegarcia_unscented.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 5
sid.inpe.br/mtc-m21/2012/07.13.14.49.46 4
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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