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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Siteplutao.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W/3RANG5H
Repositóriosid.inpe.br/plutao/2018/06.18.15.34
Última Atualização2018:06.20.14.27.02 (UTC) lattes
Repositório de Metadadossid.inpe.br/plutao/2018/06.18.15.34.55
Última Atualização dos Metadados2019:01.14.17.09.17 (UTC) administrator
Rótulolattes: 8666823357523918 3 BatistaMartMatt:2018:UsFaEm
Chave de CitaçãoBatistaMartMatt:2018:UsFaEm
TítuloOn the use of a failure emulator mechanism at nanosatellite subsystem integration tests
FormatoDVD
Ano2018
Data de Acesso26 abr. 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho433 KiB
2. Contextualização
Autor1 Batista, Carlos Leandro Gomes
2 Martins, Eliane
3 Mattiello-Francisco, Maria de Fátima
Identificador de Curriculo1
2
3 8JMKD3MGP5W/3C9JHR8
Grupo1 CRCRN-COCRE-INPE-MCTIC-GOV-BR
2
3 COCRE-COCRE-INPE-MCTIC-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Estadual de Campinas (UNICAMP)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 carlos.gomes@crn.inpe.br
2 eliane@ic.unicamp.br
3 fatima.mattiello@inpe.br
Nome do EventoIEEE Latin-American Test Symposium, 19 (LATS)
Localização do EventoSão Paulo, SP
Data12-14 mar.
Título do LivroProceedings
Tipo TerciárioPaper
Histórico (UTC)2018-06-18 15:34:55 :: lattes -> administrator ::
2018-06-19 11:34:28 :: administrator -> lattes :: 2018
2018-06-20 14:27:19 :: lattes -> administrator :: 2018
2019-01-14 17:09:17 :: administrator -> simone :: 2018
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Tipo de Versãopublisher
Palavras-Chaveinjetor de falhas
nanosatelites
robustez
canal de comunicação
ResumoThe increase number of CubeSat based space missions in the last decade shows the new possibilities for cheaper, faster but not so better projects. This lack of quality in a mission completeness point of view is associated to lack of good practices at developing, assembly and testing phases. Addressing such problem, this work presents a fault injection tool for nanosatellite robustness testing, named Failure Emulator Mechanism (FEM). The goal of the FEM is to emulate at the subsystems interface level faults that could be presented during the mission operation of the spacecraft. Working at the communication bus, the FEM is capable to intercept the exchanged messages between two subsystems under test and inject different faults: (i) time related faults, i.e. delay; (ii) value related faults, i.e. bitflip and; (iii) specific communication bus faults, i.e. a verbose subsystem. The FEM was developed to support the integration tests of the software-intensive NanoSatC-BR2 On Board Data Handling Software (OBSw) and its Payloads. The NanoSatC-BR2 is the second scientific nanosatellite developed jointly by the Brazilian National Institute for Space Researches (INPE) and Santa Maria Federal University (UFSM). As this spacecraft works with a full shared I2C communication bus, the FEM was implemented to support and work at this communication protocol and electric interface. The use of FEM has proved to be helpful along all phases of nanosatellite development. In the early phase, FEM supports robustness requirement validation by means models in the loop (MIL). In the nanosatellite integration phase, FEM supports robustness testing of the communicating subsystems under integration, configuring hardware in the loop (HIL). In this paper, we present the design, implementation and results of FEM as MIL tool for robustness requirement validation of OBSw and Langmuir Probe, a particular NanoSatC-BR2 Payload.
ÁreaETES
Arranjo 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > CRCRN > On the use...
Arranjo 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > COCRE > On the use...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
4. Condições de acesso e uso
URL dos dadoshttp://urlib.net/ibi/8JMKD3MGP3W/3RANG5H
URL dos dados zipadoshttp://urlib.net/zip/8JMKD3MGP3W/3RANG5H
Idiomaen
Arquivo Alvobatista_on.pdf
Grupo de Usuárioslattes
Grupo de Leitoresadministrator
lattes
Visibilidadeshown
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3EUAPES
8JMKD3MGPCW/3EUJHT5
Lista de Itens Citandosid.inpe.br/bibdigital/2013/10.03.20.46 1
sid.inpe.br/bibdigital/2013/10.05.15.23 1
URL (dados não confiáveis)http://ieee-ceda.org/event/19th-ieee-latin-american-test-symposium-2018
Acervo Hospedeirodpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notas
Campos Vaziosarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor isbn issn lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readpermission rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type volume
7. Controle da descrição
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