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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Sitemtc-m21d.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34T/48JSHAP
Repositóriosid.inpe.br/mtc-m21d/2023/02.23.12.44   (acesso restrito)
Última Atualização2023:02.23.12.44.37 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21d/2023/02.23.12.44.37
Última Atualização dos Metadados2023:03.28.07.29.10 (UTC) administrator
Chave SecundáriaINPE--PRE/
DOI10.1109/PRDC55274.2022.00022
ISBN978-166548555-5
ISSN15410110
Chave de CitaçãoPaivaLimCarMatMad:2022:EnSoDe
TítuloEnhanced software development process for CubeSats to cope with space radiation faults
FormatoOn-line
Ano2022
Data de Acesso17 maio 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho1771 KiB
2. Contextualização
Autor1 Paiva, David
2 Lima, Raffael Sadite Cordoville Gomes de
3 Carvalho, Manoel Jozeane Mafra de
4 Mattiello-Francisco, Maria de Fátima
5 Madeira, Henrique
Identificador de Curriculo1
2
3 8JMKD3MGP5W/3C9JHNP
4 8JMKD3MGP5W/3C9JHR8
Grupo1
2 COENE-CGGO-INPE-MCTI-GOV-BR
3 COENE-CGGO-INPE-MCTI-GOV-BR
4 COEPE-COEPE-INPE-MCTI-GOV-BR
Afiliação1 University of Coimbra
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Instituto Nacional de Pesquisas Espaciais (INPE)
5 University of Coimbra
Endereço de e-Mail do Autor1 davidpaiva.uc@gmail.com
2 raffael.sadite@inpe.br
3 manoel.j.m.carvalho@gmail.com
4 fatima.mattiello@inpe.br
5 henrique@dei.uc.pt
Nome do EventoIEEE Pacific Rim International Symposium on Dependable Computing, 27
Localização do EventoOnline
Data28 Nov. - 02 Dec. 2022
Editora (Publisher)IEEE
Páginas78-88
Título do LivroProceedings
Histórico (UTC)2023-02-23 12:46:07 :: simone -> administrator :: 2022
2023-03-28 07:29:10 :: administrator -> simone :: 2022
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-ChaveCOTS
CubeSats
fault injection
soft errors
software development
software fault tolerance techniques
verification and validation
ResumoCubeSats are an established trend in the space industry. The CubeSat standard opens opportunities for rapid and low-cost access to space. The use of COTS components instead of space-hardened hardware greatly reduces the cost of CubeSat-based missions and provides the additional benefit of increasing software functionalities at a low power consumption. However, COTS components are not designed for the space environment, making CubeSats sensitive to space radiation. This means that CubeSats need additional software mechanisms to guarantee resilient behavior in the presence of space radiation. Our proposal is that such software implemented fault tolerance mechanisms must be tailored to the specific code running in each CubeSat and the logical way to achieve that is to extend the software development process for CubeSats to include the systematic resilience evaluation of software as part of the CubeSats software lifecycle process. This paper proposes a set of structured steps to enhance the classic software development process used in CubeSats, focusing particularly on the Verification and Validation (V&V) phase. The approach uses fault injection as an integral part of the development environment for CubeSats software and includes three major steps: a) sensitivity evaluation (verification) of software in the presence of faults caused by space radiation, b) strengthen of the software with targeted software implemented fault tolerance (SWIFT) mechanisms and c) validation of the effectiveness of the SWIFT mechanisms to confirm that the software is immune to space radiation faults. These added steps to the V&V process must be carried out during software development, as well as every time the CubeSat software has an update, or even a minor change, to ensure that the impact of faults caused by space radiation is tolerated by the CubeSat software. The paper demonstrates the proposed approach using three different embedded software running in the EDC (Environment Data Collection) CubeSat board, which is part (payload) of a constellation of satellites being developed by the Brazilian National Institute for Space Research (INPE). EDC use case provides a realistic insight on the effectiveness of the proposed steps. Our results show that the proposed approach can reduce the percentage of silent data corruption (the most problematic failure mode) from the range of 15% to less than 1% and even to 0% in some embedded software, meaning that the CubeSat software becomes immune to space radiation.
ÁreaETES
Arranjo 1urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGGO > Enhanced software development...
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Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreement
agreement.html 23/02/2023 09:44 1.0 KiB 
4. Condições de acesso e uso
Idiomaen
Arquivo AlvoEnhanced_software_development_process_for_CubeSats_to_cope_with_space_radiation_faults.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Permissão de Leituradeny from all and allow from 150.163
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Repositório Espelhourlib.net/www/2021/06.04.03.40.25
Unidades Imediatamente Superiores8JMKD3MGPCW/46KUBT5
8JMKD3MGPCW/46L2EES
Lista de Itens Citandosid.inpe.br/bibdigital/2022/04.03.22.35 10
sid.inpe.br/bibdigital/2022/04.04.04.34 7
sid.inpe.br/mtc-m21/2012/07.13.14.54.30 2
Acervo Hospedeirourlib.net/www/2021/06.04.03.40
6. Notas
Campos Vaziosarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination e-mailaddress edition editor label lineage mark nextedition notes numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url volume
7. Controle da descrição
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