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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP5W34M/3FA7REQ
Repositorysid.inpe.br/mtc-m21b/2013/11.27.13.22.16   (restricted access)
Last Update2015:03.11.15.38.15 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2013/11.27.13.22.17
Metadata Last Update2021:02.11.18.12.14 (UTC) administrator
DOI10.1155/2013/257193
ISSN1024-123X
Labelisi 2013-11
Citation KeyPinheiroSouz:2013:DeMiAt
TitleDesign of the microsatellite attitude control system using the mixed H-2/H-infinity method via LMI optimization
Year2013
Access Date2024, May 02
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size2657 KiB
2. Context
Author1 Pinheiro, Erberson Rodrigues
2 Souza, Luiz Carlos Gadelha de
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
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
2 gadelha@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
Keywordscontroller performance
reliability advantages
satellite attitude control
satellite parameters
small satellite cluster
structured uncertainties
uncertainty disturbance
unstructured uncertainty
attitude control
design
DNA sequences
linear matrix inequalities
optimization
robustness (control systems)
satellites
AbstractDue to the space missions limited budget, small satellite cluster or constellation would be an economical choice. From risk-sharing viewpoint, a number of smaller satellites have a significant reliability advantage over a bigger one. Generally, one satellite is subject to two types of uncertainties: structured uncertainty that represents some satellite parameter variation and the unstructured uncertainty that represents some kind of the satellite model error. On the other hand, the Satellite Attitude Control (SAC) design becomes more vulnerable to uncertainty disturbances like model error and moment-of-inertia variation as the satellite has great decrease in size and weight. This is the case for a microsatellite with mass less than 100 kg where the ACS performance and robustness become very sensitive to both kinds of uncertainties. As a result, the design of the SAC has to deal with both types of uncertainties which is associated with the drawback between controller performance and robustness. The purpose of this work is to model a microsatellite taking into account the uncertainties and to perform the Control System Design based on the mixed H-2/H-infinity methodology via LMI optimization.
AreaETES
Arrangementurlib.net > Fonds > Produção anterior à 2021 > DIDMC > Design of the...
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4. Conditions of access and use
Languageen
User Groupadministrator
marcelo.pazos@inpe.br
Reader Groupadministrator
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Visibilityshown
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 4
sid.inpe.br/mtc-m21/2012/07.13.14.54.10 1
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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