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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP5W34M/3FA462G
Repositorysid.inpe.br/mtc-m21b/2013/11.26.17.01.44   (restricted access)
Last Update2015:03.12.13.15.40 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2013/11.26.17.01.45
Metadata Last Update2021:02.11.18.12.14 (UTC) administrator
DOI10.1155/2013/401282
ISSN1024-123X
Labelscopus 2013-11
Citation KeyKugaCarr:2013:AtDeMa
TitleAttitude determination with magnetometers and accelerometers to use in satellite simulator
Year2013
Access Date2024, May 18
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size4799 KiB
2. Context
Author1 Kuga, Helio Koiti
2 Carrara, Valdemir
Resume Identifier1 8JMKD3MGP5W/3C9JHC9
2 8JMKD3MGP5W/3C9JJAN
Group1 DMC-ETE-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)
Author e-Mail Address1 hkk@dem.inpe.br
2 val@dem.inpe.br
e-Mail Addressmarcelo.pazos@inpe.br
JournalMathematical Problems in Engineering
Volume2013
Secondary MarkB1 B1 B1 B1 B1 B2 B3 B3 B4 B4 B5
History (UTC)2021-02-11 18:12:14 :: administrator -> marcelo.pazos@inpe.br :: 2013
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAir bearing tables
Attitude accuracy
Attitude determination
Calibration method
Computer resources
Positional information
Real-time attitude
Real-time operation
Accelerometers
Algorithms
Attitude control
Bearings (machine parts)
Calibration
Magnetometers
Satellite simulators
Global positioning system
AbstractAttitude control of artificial satellites is dependent on information provided by its attitude determination process. This paper presents the implementation and tests of a fully self-contained algorithm for the attitude determination using magnetometers and accelerometers, for application on a satellite simulator based on frictionless air bearing tables. However, it is known that magnetometers and accelerometers need to be calibrated so as to allow that measurements are used to their ultimate accuracy. A calibration method is implemented which proves to be essential for improving attitude determination accuracy. For the stepwise real-time attitude determination, it was used the well-known QUEST algorithm which yields quick response with reduced computer resources. The algorithms are tested and qualified with actual data collected on the streets under controlled situations. For such street runaways, the experiment employs a solid-state magnetoresistive magnetometer and an IMU navigation block consisting of triads of accelerometers and gyros, with MEMS technology. A GPS receiver is used to record positional information. The collected measurements are processed through the developed algorithms, and comparisons are made for attitude determination using calibrated and noncalibrated data. The results show that the attitude accuracy reaches the requirements for real-time operation for satellite simulator platforms.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Attitude determination with...
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4. Conditions of access and use
Languageen
User Groupadministrator
marcelo.pazos@inpe.br
Reader Groupadministrator
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Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
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 5
sid.inpe.br/mtc-m21/2012/07.13.14.49.46 3
sid.inpe.br/mtc-m21/2012/07.13.15.01.14 2
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn lineage mark month nextedition notes number orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarymark tertiarytype url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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