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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3JJP8SL
Repositorysid.inpe.br/plutao/2015/06.01.11.54
Last Update2015:09.28.12.40.12 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2015/06.01.11.54.47
Metadata Last Update2021:02.11.18.16.37 (UTC) administrator
ISBN9783896855756
Labellattes: 1786255724025154 1 KugaBrinCarr:2015:CaStCO
Citation KeyKugaBrinCarr:2015:CaStCO
TitleAttitude estimation, control and momentum damping: a case study for CONASAT
FormatPapel
Year2015
Access Date2024, May 18
Secondary TypePRE CI
Number of Files1
Size374 KiB
2. Context
Author1 Kuga, Hélio Koiti
2 Bringhenti, Philipe M
3 Carrara, Valdemir
Resume Identifier1 8JMKD3MGP5W/3C9JHC9
2
3 8JMKD3MGP5W/3C9JJAN
Group1 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Conference Name10th International Symposium of the Academy of Astronautics: Small Satellites for Earth Observation
Conference LocationBerlim Berlin
Date2015
PublisherWissenschaft und Technik Verlag
Pages389-392
Book TitleProceedings
History (UTC)2015-06-01 11:54:47 :: lattes -> administrator ::
2021-02-11 18:16:37 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsCONASAT
attitude estimation
attitude control
momentum damping
AbstractThis paper presents the attitude estimation using Kalman filter, the PID control strategy and the momentum dumping technique using magnetorquers for the Brazilian satellite CONASAT. Attitude will be represented in quaternions, so the Kalman filter will be implemented using the reduced order covariance, to avoid the singularity of the covariance matrix. The reaction wheel desaturation will be made using the Conventional Cross Product Law (CCPL) and a bang-bang strategy, for comparison by means of the magnetorquers. The results show that the Kalman filter estimates correctly the gyroscope bias, allowing the PID controller to keep the attitude error below 5°, even during the satellite passage through the Earths shadow. The wheels speed decreased to the reference value (zero) in about 4500s, using either CCPL or the bang-bang strategy.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Attitude estimation, control...
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W/3JJP8SL
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W/3JJP8SL
Languageen
Target FileBringhenti&Carrara&Kuga - Full_Paper.pdf
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5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.49.46 1
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
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