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The search expression was <secondaryty cn and ref conference and firstg DMC-ETE-INPE-MCTI-GOV-BR and y 2012 and is *>.
2 references found looking up in 17 out of 17 Archives.
Search local date and time: 31/01/2023 07:34.
1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/3TSKB22
Repositorysid.inpe.br/mtc-m21c/2019/08.22.11.42
Last Update2019:08.22.11.42.35 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21c/2019/08.22.11.42.35
Metadata Last Update2021:02.27.04.59.59 (UTC) administrator
Secondary KeyINPE--PRE/
ISSN2316-5820
Labelself-archiving-INPE-MCTIC-GOV-BR
Citation KeyGuareschiAzKaReDuScDe:2012:CoTeBe
TitleA configurable test bed platform for test and validation of payloads for nanosatellites
Year2012
Access Date2023, Jan. 31
Secondary TypePRE CN
Number of Files1
Size661 KiB
2. Context
Author1 Guareschi, William
2 Azambuja, josé
3 Kastensmidt, Fernanda
4 Reis, Ricardo
5 Durão, Otavio Santos Cupertino
6 Schuch, Nelson Jorge
7 Dessbesel, Gustavo
Resume Identifier1
2
3
4
5 8JMKD3MGP5W/3C9JJ2L
6 8JMKD3MGP5W/3C9JHUD
Group1
2
3
4
5 DMC-ETE-INPE-MCTI-GOV-BR
6 CRS-CCR-INPE-MCTI-GOV-BR
Affiliation1 Universidade Federal do Rio Grande do Sul (UFRGS)
2 Universidade Federal do Rio Grande do Sul (UFRGS)
3 Universidade Federal do Rio Grande do Sul (UFRGS)
4 Universidade Federal do Rio Grande do Sul (UFRGS)
5 Instituto Nacional de Pesquisas Espaciais (INPE)
6 Instituto Nacional de Pesquisas Espaciais (INPE)
7 Santa Maria Design House
Author e-Mail Address1 wnguareschi@inf.ufrgs.br
2 jrfazambuja@inf.ufrgs.br
3 fglima@inf.ufrgs.br
4 reis@inf.ufrgs.br
5 otavio.durao@inpe.br
6 nelson.schuch@inpe.br
7 gustavo.dessbesel@smdh.org
EditorGonçalez, Odair Lelis
Federico, Claudio Antonio
Pereira, Marlon Antonio
Pereira, Heloisa Helena de Castilho
Conference NameWorkshop Anual Sobre os Efeitos das Radiações Ionizantes em Componentes Eletrônicos e Fotônicos de Uso Aeroespacial
Conference LocationSão José dos Campos, SP
Dateout.
PublisherInstituto de Estudos Avançados
Publisher CitySão José dos Campos
Pages18-21
Book TitleAnais
History (UTC)2019-08-22 11:43:23 :: simone -> administrator :: 2012
2021-02-27 04:59:59 :: administrator -> simone :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsNanosatellite
Cubesat
NanoSatC-BR1
FPGA
COTS
AbstractThis work proposes a design and implementation of a configurable test bed composed of communication protocols, memories and connections synthesized into a commercial flashbased FPGA for use in space applications. The intention of this platform using modular blocks is to decrease the development time and increase the flexibility and reprogrammability, when compared to ASICs circuits. The system is been designed to comply with NanoSatC-BR1 nanosatellite mission, the first Brazilian Cubesat. The FPGA will control the entire payload board. Previous in loco tests demonstrated the functionality of this configurable test bed applied to Cubesat application.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > CRCRS > A configurable test...
Arrangement 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A configurable test...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 22/08/2019 08:42 1.0 KiB 
4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W34R/3TSKB22
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W34R/3TSKB22
Languagept
Target Filegareschi_configurable.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2017/11.22.19.04.03
Next Higher Units8JMKD3MGPCW/3EUFCFP
8JMKD3MGPCW/446AF4B
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition format isbn lineage mark nextedition notes numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url volume
7. Description control
e-Mail (login)simone
update 

1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3D53MF8
Repositorydpi.inpe.br/plutao/2012/11.28.16.58
Last Update2014:01.15.10.37.46 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/11.28.16.58.20
Metadata Last Update2021:02.11.18.16.10 (UTC) administrator
Secondary KeyINPE--PRE/
ISBN21773114
Labellattes: 3095429508961900 1 SantosRocc:2012:DeFuPi
Citation KeySantosRocc:2012:DeFuPi
TitleDesign of a fuzzy pid controller for application in satellite attitude control system
FormatPapel
Year2012
Access Date2023, Jan. 31
Secondary TypePRE CN
Number of Files1
Size1464 KiB
2. Context
Author1 Santos, Willer Gomes dos
2 Rocco, Evandro Marconi
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 willer.gomes@yahoo.com.br
e-Mail Addresswiller.gomes@yahoo.com.br
Conference NameWorkshop em Engenharia e Tecnologia Espaciais, 3 (WETE).
Conference LocationSão José dos Campos
Date2012
PublisherInstituto Nacional de Pesquisas Espaciais
Volume3
Book TitleProceedings
Tertiary TypePaper
History (UTC)2012-11-28 23:06:30 :: lattes -> marciana :: 2012
2012-12-05 12:05:40 :: marciana -> administrator :: 2012
2021-02-11 18:16:10 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Keywordscontrolador PID fuzzy
sistema de controle de atitude
Fuzzy PID controller
attitude control system
AbstractIn this paper, a fuzzy proportional-integral-derivative (PID) controller is designed to be applied in the satellite attitude control system equipped with reaction wheels. An analysis of the scaling factor is developed to verify its influence during an attitude maneuver. The settling time and the pointing accuracy are the mission requirements that control system have to satisfy. The equations and theoretical concepts are introduced throughout this paper. The results showed that the adequate selection of the scaling factor contributes to the improvement of control results.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Design of a...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/3D53MF8
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/3D53MF8
Languageen
Target FileGomesW_3WETE_2012.pdf
User Groupadministrator
lattes
marciana
Reader Groupadministrator
marciana
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGP7W/3E6FERH
8JMKD3MGPCW/446AF4B
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor issn lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url versiontype
7. Description control
e-Mail (login)marciana
update