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3 referências encontradas buscando em 14 dentre 14 sites.
Data e hora local de busca: 31/10/2020 16:40.
Tipo da ReferênciaJournal Article
Identificador8JMKD3MGP3W34R/3UN3PAP
Repositóriosid.inpe.br/mtc-m21c/2020/01.07.10.02   (acesso restrito)
Metadadossid.inpe.br/mtc-m21c/2020/01.07.10.02.30
Sitemtc-m21c.sid.inpe.br
DOI10.22161/ijaers.612.42
ISSN2456-1908
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoCoicevLour:2019:PrCa
Autor1 Coicev, Marcelo
2 Loureiro, Geilson
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JH57
Grupo1 COLIT-COLIT-INPE-MCTIC-GOV-BR
2 COLIT-COLIT-INPE-MCTIC-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 marcelo.coicev@lit.inpe.br
2 geilson@lit.inpe.br
TítuloMBSE & SysML applied to the development of EGSE for satellites Assembly, Integration and Testing (AIT): a practical case
RevistaInternational Journal of Advanced Engineering Research and Science
Ano2019
Volume6
Número12
MêsDec.
Palavras-ChaveSystems Engineering, Model Based Systems Engineering, MBSE, SysML, Electrical ground Support Equipment, EGSE.
ResumoThis paper targets to present a proposal for the use of MBSE and SysML applied to a case study of the analysis in a component of a typical Electrical Ground Support Equipment (EGSE) used in Satellite Assembly, Integration and Testing (AIT). The approach aims to describe the process flow used in the analysis, providing a methodological background for the practical application of SysML notation for EGSE's development.
Páginas391-397
Idiomaen
Tipo de Trabalhojournal article
Tipo SecundárioPRE PI
AreaETES
Tamanho675 KiB
Número de Arquivos1
Arquivo Alvocoicev_mbse.pdf
Última Atualização2020:01.07.10.02.30 urlib.net/www/2017/11.22.19.04 simone
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Tipo do ConteudoExternal Contribution
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Campos Vaziosalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination e-mailaddress format isbn label lineage mark nextedition nexthigherunit notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
Data de Acesso31 out. 2020
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Tipo da ReferênciaConference Proceedings
Identificador8JMKD3MGP3W34R/3U9HMHP
Repositóriosid.inpe.br/mtc-m21c/2019/10.22.15.08
Metadadossid.inpe.br/mtc-m21c/2019/10.22.15.08.29
Sitemtc-m21c.sid.inpe.br
Chave SecundáriaINPE--PRE/
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoFernandesChisSantFraj:2019:QuInAr
Autor1 Fernandes, George
2 Chisabas, Roy Stevenson Soler
3 Santos, Márcio Bueno dos
4 Frajuca, Carlos
Identificador de Curriculo1
2
3 8JMKD3MGP5W/3C9JHPJ
Grupo1
2 COLIT-COLIT-INPE-MCTIC-GOV-BR
3 COLIT-COLIT-INPE-MCTIC-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Instituto Federal de Educação, Ciéncia e Tecnologia de São Paulo (IFSP)
Endereço de e-Mail do Autor1 georgeff.sp@gmail.com
2 roy.soler@inpe.br
3 bueno@lit.inpe.br
4 frajuca@gmail.com
TítuloQualification of an infrared array based on NICR strips for CBERS 4A satellites space simulation test
Nome do EventoInternational Astronautical Congress, 70.; IAF Space Systems Symposium
Ano2019
Data21-25 Oct.
Localização do EventoWashington, DC
ResumoDuring all development stages of a satellite project, several thermal tests are performed to confirm their functionality when exposed to the space environment. These tests must be carried out on all components, equipment or subsystems, either in engineering and flight models, or qualification and acceptance levels. These tests must meet certain specific requirements to allow the comparison with the thermal mathematical model and to evaluate the performance of the thermal control subsystem of the satellite. To perform these tests, several equipment are required such as thermal vacuum chambers, and other special apparatus to simulate the orbital thermal environment or to fulfill a particular test requirement. The Integration and Testing Laboratory - LIT, together with the Engineering and Space Technology - ETE, both from the National Institute of Space Research - INPE, in Sao Jos´e dos Campos, Brazil, designed and built an infrared array system, based on Nickel-Chrome (NiCr) strips, for simulating external orbital thermal loads during the thermal balance test of the China-Brazil Earth Resources Satellite (CBERS 04A) flight model, to be tested in acceptance levels in 2019 at LIT. This paper describes the qualification process of this apparatus, performed in 2018, as well as design parameters, materials, qualification test method, results, and all relevant information will be addressed.
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Tamanho36 KiB
Número de Arquivos1
Arquivo Alvofernandes_qualification.pdf
Última Atualização2019:10.22.15.08.29 urlib.net/www/2017/11.22.19.04 simone
Última Atualização dos Metadados2020:01.06.11.42.23 urlib.net/www/2017/11.22.19.04 administrator {D 2019}
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Histórico2019-10-22 15:08:29 :: simone -> administrator ::
2020-01-06 11:42:23 :: administrator -> simone :: 2019
Campos Vaziosaccessionnumber archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark mirrorrepository nextedition nexthigherunit notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume
Data de Acesso31 out. 2020
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Tipo da ReferênciaConference Proceedings
Identificador8JMKD3MGP3W34R/3UUMM4P
Repositóriosid.inpe.br/mtc-m21c/2020/02.17.09.44
Metadadossid.inpe.br/mtc-m21c/2020/02.17.09.44.19
Sitemtc-m21c.sid.inpe.br
Chave SecundáriaINPE--PRE/
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Chave de CitaçãoSchillingLoZhNüScMoAu:2019:InNaFo
Autor1 Schilling, K.
2 Loureiro, Geilson
3 Zhang, Y.
4 Nüchter, A.
5 Scharnagl, J.
6 Motroniuk, I.
7 Aumann, A.
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JH57
Grupo1
2 COLIT-COLIT-INPE-MCTIC-GOV-BR
Afiliação1 University Würzburg
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 China Academy of Space Technology
4 Zentrum für Telematik
5 Zentrum für Telematik
6 Zentrum für Telematik
7 Zentrum für Telematik
Endereço de e-Mail do Autor1 schi@informatik.uni-wuerzburg.de
2 geilson@lit.inpe.br
3 zhangyutu@hotmail.com
TítuloTIM: An international nano-satellite formation for photogrammetric earth observation
Nome do EventoInternational Astronautical Congress (IAC), 70
Ano2019
Título do LivroProceedings
Data21-25 Oct.
Localização do EventoWashington, MD
Palavras-ChaveNano-satellites, photogrammetry, satellite formation, sensor network.
ResumoThe objective of the Telematics International Mission (TIM) is to generate 3-dimensional images of the Earth's surface. The distributed satellite system takes advantage of different perspectives towards a given target area and uses photogrammetric methods. Here by distributed control technologies a formation/constellation of 9 cooperating small satellites is realized. The application scenario focusses on characterization of ash clouds from volcano eruptions, addressing ash distribution profiles in different heights. This provides useful information to plan detour maneuvers for airplanes to avoid damage for engines.
Idiomaen
Tipo SecundárioPRE CI
AreaETES
Última Atualização dos Metadados2020:02.17.09.45.15 urlib.net/www/2017/11.22.19.04 simone {D 2019}
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simone
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Tipo do ConteudoExternal Contribution
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agreement.html 17/02/2020 06:44 1.0 KiB 
Campos Vaziosaccessionnumber archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn label lineage mark nextedition nexthigherunit notes numberoffiles numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readpermission rightsholder secondarydate secondarymark serieseditor session shorttitle size sponsor subject targetfile tertiarymark tertiarytype type url versiontype volume
Data de Acesso31 out. 2020
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