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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP5W34M/3HE6FC6
Repositorysid.inpe.br/mtc-m21b/2014/11.18.23.57.49   (restricted access)
Last Update2015:02.09.11.59.53 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2014/11.18.23.57.50
Metadata Last Update2021:02.11.18.12.20 (UTC) administrator
DOI10.1155/2014/260206
ISSN1070-9622
Labelscopus 2014-11 SouzaSouz:2014:SaAtCo
Citation KeySouzaSouz:2014:SaAtCo
TitleSatellite attitude control system design considering the fuel slosh dynamics
Year2014
Access Date2024, May 19
Secondary TypePRE PI
Number of Files1
Size2548 KiB
2. Context
Author1 Souza, Luiz Carlos Gadelha de
2 Souza, Alain Giacobini De
Resume Identifier1 8JMKD3MGP5W/3C9JHN3
Group1 DMC-ETE-INPE-MCTI-GOV-BR
2 CMC-ETES-SPG-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
e-Mail Addressmarcelo.pazos@inpe.br
JournalShock and Vibration
Volume2014
Secondary MarkB1_INTERDISCIPLINAR B1_ENGENHARIAS_III B1_ENGENHARIAS_I B2_ENGENHARIAS_IV
History (UTC)2021-02-11 18:12:20 :: administrator -> marcelo.pazos@inpe.br :: 2014
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsCommunication satellites
Controllers
Design
Dynamics
Fuel tanks
Navigation
Controller performance
Flexible solar panels
Kalman filter technique
Linear quadratic Gaussian
Linear quadratic regulator
Mechanical manipulators
Satellite attitude control systems
Satellite structure
Satellite antennas
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. A crucial interaction can occur between the fuel slosh motion and the satellite rigid motion during translational and/or rotational manoeuvre since these interactions can change the satellite centre 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 thus affecting the satellite attitude acquisition. 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 satellite dynamics in order to predict what the damage to the controller performance and robustness is. The fuel slosh dynamics is modelled by a pendulum which parameters are identified using the Kalman filter technique. This information is used to design the satellite controller by the linear quadratic regulator (LQR) and linear quadratic Gaussian (LQG) methods to perform a planar manoeuvre assuming thrusters are actuators. © 2014 Luiz Carlos Gadelha de Souza and Alain G. de Souza.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Satellite attitude control...
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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
LinkingTrabalho não Vinculado à Tese/Dissertação
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 7
sid.inpe.br/mtc-m21/2012/07.13.14.54.10 4
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 electronicmailaddress 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 tertiarytype typeofwork url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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