1. Identificação | |
Tipo de Referência | Artigo em Evento (Conference Proceedings) |
Site | mtc-m21b.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W34P/3L9LCKH |
Repositório | sid.inpe.br/mtc-m21b/2016/03.03.15.16 |
Última Atualização | 2016:05.04.18.19.05 (UTC) administrator |
Repositório de Metadados | sid.inpe.br/mtc-m21b/2016/03.03.15.16.38 |
Última Atualização dos Metadados | 2022:08.22.23.17.05 (UTC) administrator |
Chave Secundária | INPE--PRE/ |
Chave de Citação | ConceiçãoAmbrMatt:2016:UsNATe |
Título | On the use of NANOSATC-BR test system for payload operational requirements verification |
Ano | 2016 |
Data de Acesso | 24 abr. 2024 |
Tipo Secundário | PRE CI |
Número de Arquivos | 1 |
Tamanho | 625 KiB |
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2. Contextualização | |
Autor | 1 Conceição, Carlos 2 Ambrosio, Ana Maria 3 Mattiello Francisco, Maria de Fátima |
Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JGH7 3 8JMKD3MGP5W/3C9JHR8 |
Grupo | 1 2 DSE-ETE-INPE-MCTI-GOV-BR 3 CCR-CCR-INPE-MCTI-GOV-BR |
Afiliação | 1 Instituto de Aeronáutica e Espaço (IAE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) |
Endereço de e-Mail do Autor | 1 carloscaplc@iae.cta.br 2 ana.ambrosio@inpe.br 3 fatima.mattiello@inpe.br |
Nome do Evento | Latin American IAA CubeSat Workshop, 2 |
Localização do Evento | Florianópolis, SC |
Data | 28 Feb. - 02 Mar. |
Histórico (UTC) | 2016-03-03 15:16:38 :: simone -> administrator :: 2016-06-04 05:08:15 :: administrator -> simone :: 2016 2016-06-20 12:46:13 :: simone -> administrator :: 2016 2021-02-11 20:57:55 :: administrator -> simone :: 2016 2022-04-11 18:05:55 :: simone -> administrator :: 2016 2022-08-22 23:17:05 :: administrator -> simone :: 2016 |
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3. Conteúdo e estrutura | |
É a matriz ou uma cópia? | é a matriz |
Estágio do Conteúdo | concluido |
Transferível | 1 |
Tipo do Conteúdo | External Contribution |
Resumo | The need for a global quick and efficient communication, observation and understanding of events on Earth and conquest of space, motivates spacetechnology development. The CubeSat standard, also known as U-Classnanosatellite platform, has enabled the flight qualification of innovativespace technologies developed in academic environment and / or emergingcompanies in the sector. For over three decades leading research anddevelopment satellites in Brazil, the National Institute for Space Research(INPE) has supported over the past five years the development ofnanosatellites projects in INPE´s regional centers at Northeast and South of Brazil in cooperation with local universities. In this context, NanosatC-Brfamily has been developed. First satellite, NanosatC-Br1, is a 1U Cubesat launched in July 2014 for purposing of both collecting the Earth's magnetic field data and measuring in flight the radiation resilience of integrated circuits designed in Brazil. The qualification of embedded software systems is one of the main challenges of the second mission, a 2U Cubesat named NanosatC-Br2 that is planned to be launched in 2016. The use of existing components on the market (COTS) added to the standardization of on board subsystems in nanosatellites platforms have allowed to reduce significantly the space mission development cycle enabling new space technologies being qualified on flight at low-cost. However, the verification and validation activities (V&V) at different stages of the space project lifecycle are still required and onerous in terms of resources and time. At least functional and dependability aspects of the payload integration with the satellite platform need to be systemically tested. Aiming to avoid the development of new test environment every new mission of a nanosatellite family, which spends time, hardware and software resources, this article presents a reusable Test System for NanosSatC-BR family. The reusability issues of Test System are addressed in two perspectives: (i) reuse the Test System at different stages of the same mission; (ii) reuse the Test System in different satellites of the same family. The proposed Test System architecture supports the V&V process focusing on interoperability features between the NanosatC-Br onboard computer and its payloads, aided by fault injection mechanisms. |
Área | ETES |
Arranjo 1 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > COCRE > On the use... |
Arranjo 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDSE > On the use... |
Conteúdo da Pasta doc | acessar |
Conteúdo da Pasta source | não têm arquivos |
Conteúdo da Pasta agreement | |
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4. Condições de acesso e uso | |
URL dos dados | http://urlib.net/ibi/8JMKD3MGP3W34P/3L9LCKH |
URL dos dados zipados | http://urlib.net/zip/8JMKD3MGP3W34P/3L9LCKH |
Arquivo Alvo | conceicao.pdf |
Grupo de Usuários | simone |
Grupo de Leitores | administrator simone |
Visibilidade | shown |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Repositório Espelho | urlib.net/www/2011/03.29.20.55 |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/3EUJHT5 8JMKD3MGPCW/446AUSL |
Lista de Itens Citando | sid.inpe.br/bibdigital/2021/02.11.20.54 2 sid.inpe.br/mtc-m21/2012/07.13.14.39.50 1 sid.inpe.br/bibdigital/2013/10.05.15.23 1 |
Acervo Hospedeiro | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
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6. Notas | |
Campos Vazios | archivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label language lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume |
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7. Controle da descrição | |
e-Mail (login) | simone |
atualizar | |
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