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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3HG7CLE
Repositorysid.inpe.br/plutao/2014/12.01.12.07.51   (restricted access)
Last Update2015:02.11.16.52.53 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2014/12.01.12.07.52
Metadata Last Update2021:02.11.18.11.24 (UTC) administrator
ISSN0065-3438
Labellattes: 0288494962313241 1 CarraraOlivKuga:2014:GaBePl
Citation KeyCarraraOlivKuga:2014:GaBePl
TitleA gas bearing platform attitude control for assessment of AOCS systems
Year2014
Access Date2024, May 18
Secondary TypePRE PI
Number of Files1
Size896 KiB
2. Context
Author1 Carrara, Valdemir
2 Oliveira, Alexandre Macedo de
3 Kuga, Helio Koiti
Resume Identifier1 8JMKD3MGP5W/3C9JJAN
2
3 8JMKD3MGP5W/3C9JHC9
Group1 DMC-ETE-INPE-MCTI-GOV-BR
2
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 val@dem.inpe.br
2
3 helio.kuga@inpe.br
e-Mail Addressmarcelo.pazos@inpe.br
JournalAdvances in the Astronautical Sciences
Volume152
Number1
Pages2677-2695
History (UTC)2014-12-01 12:07:52 :: lattes -> administrator ::
2021-02-11 18:11:24 :: 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
Keywordsair bearing
Attitude control
Attitude dynamics
Extended Kalman Filter
AbstractThis paper presents a solution for the development, validation and testing of attitude control system for satellites with hardware-in-the-loop dynamics and control. The system is based on a gas-bearing platform in which several sensors and actuators, similar to those usually employed in satellites (engineering models) were fixed. Magnetometers and gyroscopes are easily incorporated to the platform, but sun sensors and star sensors are more difficult. The solar sensors are replaced by a tri-axes accelerometer, while the star sensor relies on direct night sky measurements. Although hot gas thrusters cannot be used, both magnetic torque coils and reaction wheels are feasible to be incorporated to the arrangement. The gas-bearing balancing process is critical for real satellite dynamic simulation and therefore the solution is addressed in this work, by means of a non-linear filtering of the sensor readings. The filtering process also obtains the platform mass properties. In order to increase the filter accuracy the gyroscopes were calibrated; the calibration results are also presented here. Finally, an attitude controller was implemented in the platform and the control performance was analyzed and shown together with the conclusions.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A gas bearing...
doc Directory Contentaccess
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4. Conditions of access and use
Languageen
Target FileCarrara_Gas.pdf
User Grouplattes
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
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Read Permissiondeny from all and allow from 150.163
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
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 3
sid.inpe.br/mtc-m21/2012/07.13.14.49.46 1
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi format isbn lineage mark month nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarytype typeofwork url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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