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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3E7UDK8
Repositorydpi.inpe.br/plutao/2013/05.31.17.07
Last Update2013:07.17.11.47.05 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2013/05.31.17.07.03
Metadata Last Update2021:02.11.18.16.11 (UTC) administrator
Labellattes: 1786255724025154 1 KugaCarr:2013:AtDeMa
Citation KeyKugaCarr:2013:AtDeMa
TitleAttitude determination with magnetometers and accelerometers to use in satellite simulator
FormatDVD
Year2013
Access Date2024, May 18
Secondary TypePRE CI
Number of Files1
Size3061 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 Addresshkk@dem.inpe.br
Conference NameInternational Symposium on Dynamic Problems of Mechanics, 15 (DINAME).
Conference LocationBuzios
Date2013
PublisherABCM
Book TitleProceedings
Tertiary TypePaper
History (UTC)2013-05-31 17:17:02 :: lattes -> administrator :: 2013
2013-07-17 12:00:48 :: administrator -> marcelo.pazos@sid.inpe.br :: 2013
2014-01-10 14:00:43 :: marcelo.pazos@sid.inpe.br -> administrator :: 2013
2021-02-11 18:16:11 :: 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
Keywordsattitude determination
quest algorithm
satellite simulator
magnetometer
accelerometer
AbstractSystems of attitude control of artificial satellites are dependent on a reference attitude, provided by an attitude determination process. This paper presents the implementation and tests of a fully self-contained algorithm for the determination of attitude using magnetometer and accelerometer units, for application on a satellite attitude simulator based on frictionless air bearing tables. However it is known that magnetometers and accelerometers need to be calibrated so as to allow that such measurements are used to their ultimate accuracy. A calibration method is implemented which proves to be an essential part of the procedure to achieve better 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 an Honeywell (solid-state magneto-resistive technology) magnetometer HMR-2300 and a Crossbow (Xbow-CD-400) IMU navigation block consisting of a triad of accelerometers and a triad of gyros, with MEMS technology. A GPS receiver is used to obtain positional information. The collected measurements are processed through the developed algorithms, and comparisons are made for attitude determination using calibrated and non-calibrated data. The results show that the implemented process of attitude determination reaches the requirements for real-time operation with enough accuracy to a regular standby or emergency mode operation.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Attitude determination with...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/3E7UDK8
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/3E7UDK8
Languageen
Target FileDINAME33.pdf
User Groupbanon
lattes
marcelo.pazos@inpe.br
self-uploading-INPE-MCTI-GOV-BR
Reader Groupadministrator
banon
marcelo.pazos@inpe.br
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/446AF4B
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor isbn issn lineage mark nextedition numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url volume
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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