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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3FCL86P
Repositorysid.inpe.br/plutao/2013/12.12.16.11.27
Last Update2015:03.10.18.28.11 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2013/12.12.16.11.28
Metadata Last Update2021:02.11.18.16.26 (UTC) administrator
Labellattes: 5801699053436537 2 SouzaSouz:2013:DESAAT
Citation KeySouzaSouz:2013:DeSaAt
TitleDesign of satellite attitude control system considering the interaction between fuel slosh and flexible dynamics
Year2013
Access Date2024, May 20
Secondary TypePRE CI
Number of Files1
Size349 KiB
2. Context
Author1 Souza, Alain Giacobini de
2 Souza, Luiz Carlos Gadelha de
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
Group1 CMC-ETES-SPG-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 luiz.souza@inpe.br
e-Mail Addressluiz.souza@inpe.br
Conference NameInternational Conference on Vibration Problems, 11 (ICOVP).
Conference LocationLisboa
Date2013
PublisherIdMEC
Volume1
Pages212-218
Book TitleProceedings
Tertiary TypePaper
History (UTC)2013-12-12 16:11:28 :: lattes -> administrator ::
2021-02-11 18:16:26 :: 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
KeywordsFUEL SLOSH AND FLEXIBLE DYNAMICS
Control System Design
AbstractThe design of the satellite Attitude Control System (ACS) becomes more complex when the satellite structure has different type of components like, flexible solar panels, antennas, mechanical manipulators and tanks with fuel, since the ACS performance and robustness will depend if the dynamics interaction effects between these components are considered in the satellite controller design. A crucial interaction can occur between the fuel slosh motion and the satellite rigid motion during translational and/or rotational maneuver since these interactions can change the satellite center of mass position damaging the ACS pointing accuracy. Although, a well-designed controller can suppress such disturbances quickly, the controller error pointing may be limited by the minimum time necessary to suppress such disturbances affecting thus the satellite attitude acquisition. It is known that one way to minimize such problems is to design controllers with a bandwidth below the lowest slosh and/or vibration mode which can result in slow maneuvers inconsistent with the space mission requirements. As a result, the design of the satellite controller needs to explore the limits between the conflicting requirements of performance and robustness. This paper investigates the effects of the interaction between the liquid motion (slosh) and the flexible satellite dynamics in order to predict what the damage to the controller performance and robustness is. The fuel slosh dynamics is modeled using its pendulum analogs mechanical system which parameters are identified using the Kalman filter technique. This information is used to designs and to compare the satellite attitude control system by the Linear Quadratic Gaussian (LQG) and Hinfinity methods.
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W/3FCL86P
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W/3FCL86P
Languageen
Target FileSouza_design.pdf
User Grouplattes
marcelo.pazos@inpe.br
Reader Groupadministrator
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/3F2UALS
8JMKD3MGPCW/446AF4B
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Outras atividades profissionais, científicas e técnicas.
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor format isbn issn lineage mark nextedition numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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