Close

1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3HG7BP2
Repositorysid.inpe.br/plutao/2014/12.01.11.56.51
Last Update2015:02.11.12.54.09 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2014/12.01.11.56.52
Metadata Last Update2021:02.11.18.16.33 (UTC) administrator
Labellattes: 1786255724025154 2 GarciaKugaZanaMato:2014:ATESPR
Citation KeyGarciaKugaZanaMato:2014:AtEsPr
TitleAttitude estimation process of the sensing remote satellite cbers-2 with unscented kalman filter and quaternion incremental, using real data
FormatDVD
Year2014
Access Date2024, May 18
Secondary TypePRE CI
Number of Files1
Size643 KiB
2. Context
Author1 Garcia, Roberta Veloso
2 Kuga, Hélio Koiti
3 Zanardi, Maria Cecilia França de Paula Santos
4 Matos, Nicholas de Freitas Oliveira
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)
4 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1
2 helio.kuga@inpe.br
e-Mail Addressmarcelo.pazos@inpe.br
Conference NameInternational Symposium on Space Flight Dynamics, 24 (ISSFD).
Conference LocationLaurel
Date2014
PublisherJohns Hopkins - Applied Physics Laboratory
Pages1-15
Book TitleProceedings
Tertiary TypePaper
History (UTC)2014-12-01 11:56:52 :: lattes -> administrator ::
2021-02-11 18:16:33 :: administrator -> marcelo.pazos@inpe.br :: 2014
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsUnscented Kalman filter
attitude estimation
quaternions
extended Kalman filter
AbstractThis work is related to the dynamics of rotational motion of artificial satellites, that is, its orientation (attitude) with respect to an inertial reference system. The attitude determination process, in general, involves the knowledge of nonlinear estimation techniques and is essential to the safety and control of the satellite and payload. The aim of this work is to study the influence of real data of the CBERS-2 (China Brazil Earth Resources Satellite) satellite in the attitude estimation process when the estimator is the Unscented Kalman Filter (UKF) and the attitude is represented by quaternion incremental. The attitude sensors available are DSS (Digital Sun Sensor), IRES (Infrared Earth Sensor), and the gyros. For nonlinear systems, the UKF uses a carefully selected set of sample points to map the probability distribution more accurately than the linearization of the standard Extended Kalman Filter (EKF). Herein the proposal is to estimate the attitude and the drift of the gyros obtained by the UKF and EKF with quaternion incremental and compare them. The results show that, although the EKF and UKF have roughly the same accuracy, the UKF leads to a convergence of the state vector faster than the EKF. This fact was expected, since the UKF prevents the linearizations needed for EKF, when the system has some nonlinearity in their equations.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Attitude estimation process...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W/3HG7BP2
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W/3HG7BP2
Languageen
User Grouplattes
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
LinkingTrabalho não Vinculado à Tese/Dissertação
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/446AF4B
URL (untrusted data)https://dnnpro.outer.jhuapl.edu/Portals/35/ISSFD24_Paper_Release/ISSFD24_Paper_S4-3_VelosoGarcia.doc
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor isbn issn lineage mark nextedition numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject targetfile type volume
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
update 


Close