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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3J9R4EP
Repositorysid.inpe.br/mtc-m21b/2015/04.07.13.20
Last Update2015:04.07.13.22.42 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2015/04.07.13.20.59
Metadata Last Update2021:02.11.18.19.45 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeyOliveiraKugaCarr:2015:AiBePl
TitleAir bearing platforms for simulation of spacecraft attitude control systems
Year2015
Access Date2024, May 18
Secondary TypePRE CI
Number of Files1
Size1919 KiB
2. Context
Author1 Oliveira, Alexandre Macedo de
2 Kuga, Hélio Koiti
3 Carrara, Valdemir
Resume Identifier1
2 8JMKD3MGP5W/3C9JHC9
3 8JMKD3MGP5W/3C9JJAN
Group1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 alexandre.oliveira@inpe.br
2 helio.kuga@inpe.br
3 valdemir.carrara@inpe.br
EditorSteffen Junior, V.
Rade, D. A.
Bessa, W. M.
Conference NameInternational Symposium on Dynamic Problems of Mechanics, 17.
Conference LocationNatal, RN
Date22-27 Feb.
PublisherABCM
Book TitleProceedings
History (UTC)2015-04-07 13:20:59 :: simone -> administrator ::
2021-02-11 18:19:45 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typefinaldraft
Keywordsair bearing
attitude control
satellite simulator
Kalman filter
inertial systems
AbstractThis paper presents the development of two different air bearing tables, which can simulate attitude control systems for satellites with hardware-in-the-loop dynamics and control. Both systems are based on gas-bearing platforms in which several sensors and actuators were fixed. The first platform has a MEMS inertial sensor, and the second platform has several sensors and actuators that are engineering models similar to those usually employed in satellites. A PC/104 computer commands the first platform, which is responsible for driving 8 cold gas thrusters. On the other hand, the second platform is based on a Renesas 32 bits processor, which is responsible for three different subsystems: power supply, data handling and attitude control. The actuators in this case are reaction wheels and magnetic torque coils. The most important process for the correct operation of the simulators is to ensure accurate balancing of both platforms, because a difference between the center of gravity of the platform and the center of rotation of the bearing support may generate higher torques than those normally encountered in the space environment, invalidating the main feature of the simulator. Therefore, we use non-linear filtering to obtain the platforms mass properties, including the center of gravity position. Finally, we validate the mass properties by implementing two simple attitude stabilization controllers. Considerations on the nature of the friction of the two platforms will also be made in the end of this paper.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Air bearing platforms...
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4. Conditions of access and use
data URLhttp://mtc-m21b.sid.inpe.br/ibi/8JMKD3MGP3W34P/3J9R4EP
zipped data URLhttp://mtc-m21b.sid.inpe.br/zip/8JMKD3MGP3W34P/3J9R4EP
Languageen
Target Fileoliveira_air.PDF
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Linking8JMKD3MGP5W34M/3GK4L3P
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 2
sid.inpe.br/mtc-m21/2012/07.13.15.01.14 1
sid.inpe.br/mtc-m21b/2013/09.26.14.25.22 1
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition format isbn issn label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarytype type url volume
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