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1. Identity statement
Reference TypeJournal Article
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/3EGJFCL
Repositorysid.inpe.br/mtc-m19/2013/07.23.19.24
Last Update2013:07.25.14.35.00 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19/2013/07.23.19.24.26
Metadata Last Update2021:02.11.18.10.34 (UTC) administrator
DOI10.1155/2013/318072
ISSN2314-4904
2314-4912
Citation KeySouzaAren:2013:DeSaAt
TitleDesign of satellite attitude control algorithm based on the SDRE method using gas jets and reaction wheels
Year2013
Access Date2024, May 19
Secondary TypePRE PI
Number of Files1
Size3150 KiB
2. Context
Author1 Souza, Luiz Carlos Gadelha de
2 Arena, Victor Massad Ruiz
Resume Identifier1 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 gadelha@dem.inpe.br
e-Mail Addressmarcelo.pazos@inpe.br
JournalJournal of Engineering
Volume2013
Pages318072
History (UTC)2013-07-23 19:24:26 :: marcelo.pazos@sid.inpe.br -> administrator ::
2021-02-11 18:10:34 :: 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
Keywordssatellite attitude control algorithm
SDRE method
gas jets
reaction wheel torque
space mission cost
angle maneuver
LQR linear controller
SDRE filter
DMC 3D satellite simulator
state-dependent Riccati equation
plant nonlinearities
system noise
angular velocity reduction
switching control algorithm
minimum system energy
AbstractAn experimental attitude control algorithm design using prototypes can minimize space mission costs by reducing the number of errors transmitted to the next phase of the project. The Space Mechanics and Control Division (DMC) of INPE is constructing a 3D simulator to supply the conditions for implementing and testing satellite control hardware and software. Satellite large angle maneuver makes the plant highly nonlinear and if the parameters of the system are not well determined, the plant can also present some level of uncertainty. As a result, controller designed by a linear control technique can have its performance and robustness degraded. In this paper the standard LQR linear controller and the SDRE controller associated with an SDRE filter are applied to design a controller for a nonlinear plant. The plant is similar to the DMC 3D satellite simulator where the unstructured uncertainties of the system are represented by process and measurements noise. In the sequel the State-Dependent Riccati Equation (SDRE) method is used to design and test an attitude control algorithm based on gas jets and reaction wheel torques to perform large angle maneuver in three axes. The SDRE controller design takes into account the effects of the plant nonlinearities and system noise which represents uncertainty. The SDRE controller performance and robustness are tested during the transition phase from angular velocity reductions to normal mode of operation with stringent pointing accuracy using a switching control algorithm based on minimum system energy. This work serves to validate the numerical simulator model and to verify the functionality of the control algorithm designed by the SDRE method.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Design of satellite...
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP7W/3EGJFCL
zipped data URLhttp://urlib.net/zip/8JMKD3MGP7W/3EGJFCL
Languageen
Target File318072.pdf
User Groupmarcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
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/mtc-m21/2012/07.13.14.54.10 4
sid.inpe.br/bibdigital/2021/02.11.18.06 3
URL (untrusted data)http://dx.doi.org/10.1155/2013/318072
DisseminationPORTALCAPES
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn label lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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