Close

1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3KN355B
Repositorysid.inpe.br/plutao/2015/12.04.14.04.48   (restricted access)
Last Update2015:12.09.15.12.50 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2015/12.04.14.04.49
Metadata Last Update2021:07.28.22.22.43 (UTC) administrator
DOI10.1088/1742-6596/641/1/012005
ISSN1742-6588
Labellattes: 7752228013890691 1 SilvaKugaZana:2015:NoLeSq
Citation KeySilvaKugaZana:2015:NoLeSq
TitleNonlinear least squares method for gyros bias and attitude estimation using satellite attitude and orbit toolbox for matlab
Year2015
Access Date2024, May 18
Secondary TypePRE PI
Number of Files1
Size1064 KiB
2. Context
Author1 Silva, William Reis
2 Kuga, Hélio Koiti
3 Zanardi, Maria Cecília Franca de Paula Santos
Resume Identifier1
2 8JMKD3MGP5W/3C9JHC9
Group1 CMC-ETES-SPG-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Federal do ABC (UFABC)
Author e-Mail Address1 reis.william@gmail.com
2 helio.kuga@inpe.br
JournalJournal of Physics: Conference Series
Volume641
Pages012005
Secondary MarkB2_INTERDISCIPLINAR B2_ENGENHARIAS_III B3_MEDICINA_II B3_GEOCIÊNCIAS B4_MATERIAIS B4_ENGENHARIAS_II B4_BIOTECNOLOGIA C_QUÍMICA C_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA C_ENGENHARIAS_IV C_ECONOMIA C_ASTRONOMIA_/_FÍSICA
History (UTC)2015-12-04 14:04:49 :: lattes -> administrator ::
2021-07-28 22:22:43 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsNonlinear Least Squares
Attitude Estimation
Gyros drift
AbstractThe knowledge of the attitude determination is essential to the safety and control of the satellite and payload, and this involves approaches of nonlinear estimation techniques. Here one focuses on determining the attitude and the gyros drift of a real satellite CBERS-2 (China Brazil Earth Resources Satellite) using simulated measurements provided by propagator PROPAT Satellite Attitude and Orbit Toolbox for Matlab. The method used for the estimation was the Nonlinear Least Squares Estimation (NLSE). The attitude dynamical model is described by nonlinear equations involving the Euler angles. The attitude sensors available are two DSS (Digital Sun Sensor), two IRES (Infra-Red Earth Sensor), and one triad of mechanical gyros. The two IRES give direct measurements of roll and pitch angles with a certain level of error. The two DSS are nonlinear functions of roll, pitch, and yaw attitude angles. Gyros are very important sensors, as they provide direct incremental angles or angular velocities. However gyros present several sources of error of which the drift is the most troublesome. Results show that one can reach accuracies in attitude determination within the prescribed requirements, besides providing estimates of the gyro drifts which can be further used to enhance the gyro error model.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Nonlinear least squares...
Arrangement 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Nonlinear least squares...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target File1_silva5.pdf
User Grouplattes
simone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 3
URL (untrusted data)http://dx.doi.org/10.1088/1742-6596/641/1/012005
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Description control
e-Mail (login)simone
update 


Close