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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3C63NL3
Repositorydpi.inpe.br/plutao/2012/06.21.19.01.13
Last Update2012:08.24.16.24.24 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/06.21.19.01.14
Metadata Last Update2021:02.11.18.11.13 (UTC) administrator
DOI10.3233/SAV-2012-0702
ISSN1070-9622
Labellattes: 5801699053436537 2 Mainenti-LopesSouzSous:2012:DeNoCo
Citation KeyMainenti-LopesSouzSous:2012:DeNoCo
TitleDesign of a nonlinear controller for a rigid-flexible satellite using multi-objective Generalized Extremal Optimization with real codification
Year2012
Access Date2024, May 19
Secondary TypePRE PI
Number of Files1
Size494 KiB
2. Context
Author1 Mainenti-Lopes, Igor
2 Souza, Luiz Carlos Gadelha de
3 Sousa, Fabiano Luis de
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
3 8JMKD3MGP5W/3C9JH3H
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 gadelha@dem.inpe.br
e-Mail Addressgadelha@dem.inpe.br
JournalShock and Vibration
Volume19
Number5
Pages1-10
Secondary MarkB1_ENGENHARIAS_I B1_ENGENHARIAS_III B2_ENGENHARIAS_IV B1_INTERDISCIPLINAR
History (UTC)2012-06-22 00:10:59 :: lattes -> secretaria.cpa@dir.inpe.br :: 2012
2012-08-24 16:24:24 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012
2012-10-19 20:26:57 :: administrator -> secretaria.cpa@dir.inpe.br :: 2012
2012-12-14 11:59:05 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012
2021-02-11 18:11:13 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typefinaldraft
KeywordsDynamic and control of flexible system
optimization algorithm
AbstractThe Attitude Control System (ACS) for Flexible Space Structures (FSS) like rigid-flexible satellite and solar sails demands great reliability, autonomy and robustness. The association of flexible motion and large angle maneuver imply that the FSS dynamics is only captured by complex non-linear mathematical model. As a result, FSS controller performance designed by linear control technique under the hypothesis of rigid dynamic can be degraded. Although vibrations can be suppressed rapidly, the flexibility effect can introduce a tracking error resulting in a minimum attitude acquisition time. On the other hand, faster manoeuvres can excite flexible modes in such a way to make the FSS lose the required pointing accuracy. In the present work, it is shown that a new multi-objective optimization algorithm, called M-GEOreal (Multi-objective Generalized Extremal Optimization with real codification), is a good tool to be used in such kind of problems. The M-GEOreal is a real coded version of the M-GEO evolutionary algorithm. Its performance on finding the gains of a non linear control law is evaluated through its application to the problem of controlling a large angle attitude manoeuvre of a rigid-flexible satellite. The satellite non-linear model consists of a rigid central hub with a clamped free flexible beam. The multi-objective approach allows optimizing conflicting objective functions like time and energy. As a result, one can find a trade-off solution (non-dominated solutions). These solutions become available to the designer for posterior choice of an individual solution to be implemented. The non-dominated solutions are represented in the design space (Pareto set) and in the objective functions space (Pareto front). Having in mind the complexity of implementing a control algorithm in onboard satellite computer, this preliminary investigation has shown that the non-linear controller based on the M-GEOreal algorithm is a promising technique, since it has satisfied all the ACS requirements. A great advantage of the M-GEOreal procedure is its capacity to deal with non-linear system and designing non-linear controller with constant gains facilitating the on board computer implementation.
AreaETES
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/3C63NL3
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/3C63NL3
Languageen
Target Filefulltext.pdf
User Groupadministrator
lattes
secretaria.cpa@dir.inpe.br
Reader Groupadministrator
secretaria.cpa@dir.inpe.br
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
LinkingTrabalho Vinculado à Tese/Dissertação
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 2
DisseminationWEBSCI; PORTALCAPES.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Atividades profissionais, científicas e técnicas.
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn lineage mark mirrorrepository month nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarytype typeofwork url
7. Description control
e-Mail (login)marciana
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