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1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Sitemtc-m21c.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34R/3T3HUJS
Repositóriosid.inpe.br/mtc-m21c/2019/04.02.17.01   (acesso restrito)
Última Atualização2019:04.02.17.01.29 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21c/2019/04.02.17.01.29
Última Atualização dos Metadados2020:01.06.11.42.12 (UTC) administrator
DOI10.1016/j.actaastro.2018.11.011
ISSN0094-5765
Chave de CitaçãoBatistaWellMartMatt:2019:ToInNa
TítuloTowards increasing nanosatellite subsystem robustness
Ano2019
MêsMar.
Data de Acesso09 maio 2024
Tipo de Trabalhojournal article
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho1407 KiB
2. Contextualização
Autor1 Batista, Carlos Leandro Gomes
2 Weller, Anderson Coelho
3 Martins, Eliane
4 Mattiello Francisco, Maria de Fátima
Identificador de Curriculo1
2
3
4 8JMKD3MGP5W/3C9JHR8
Grupo1 CSE-ETES-SESPG-INPE-MCTIC-GOV-BR
2
3
4 COCRE-COCRE-INPE-MCTIC-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Estadual de Campinas (UNICAMP)
3 Universidade Estadual de Campinas (UNICAMP)
4 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 carlos.batista@ieee.org
2
3
4 fatima.mattiello@inpe.br
RevistaActa Astronautica
Volume156
Páginas187-196
Nota SecundáriaA2_INTERDISCIPLINAR B1_GEOCIÊNCIAS B1_ENGENHARIAS_IV B1_ENGENHARIAS_III B2_CIÊNCIA_DA_COMPUTAÇÃO C_ENGENHARIAS_II C_ASTRONOMIA_/_FÍSICA
Histórico (UTC)2019-04-02 17:01:29 :: simone -> administrator ::
2019-04-02 17:01:29 :: administrator -> simone :: 2019
2019-04-02 17:02:07 :: simone -> administrator :: 2019
2020-01-06 11:42:12 :: administrator -> simone :: 2019
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-ChaveFault injection
Robustness
Testing
Verification and validation
Nanosatellite
Cubesat
Integration
MIL
ResumoShort development life cycle and low cost of cubesat-based mission have motivated the growing number of nanosatellite launched in the last decade around the world. Fast and cheaper space project do not guarantee success in orbit. The lack of good practices on design, assembly and tests has been pointed out as one of the major causes to nanosatellite mission failures. Efforts on the use of verification and validation techniques are required. Because the increased use of nanosatellites missions for technology qualification of payloads on orbit, faulty behavior of those payloads can be expected. However, such malfunction shall not represent a risk to the whole mission. Robustness is an important property of reactive critical system not addressed properly in the cubesat standardization. Although significant mitigation of the interface failures has been observed at hardware level in the integration phase of the payloads with the nanosatellite platform, behavior aspects of the communicating subsystems on the use of these interfaces shall be verified. The test systematization of CubeSat-based nanosatellites supported by proper tools is necessary to reduce the mission development cycle in terms of the time consumed by the verification & validation activities. In this paper we present a failure emulator mechanism framework, named FEM, for robustness testing of interoperable software-intensive subsystems onboard nanosatellite. FEM acts in the communication channel being part of the integration test workbench in two phases of nanosatellite design: (i) robustness requirement specification using model in the loop (MIL) and (ii) robustness validation using hardware in the loop (HIL). The architectural aspects of the proposed FEM framework support its instantiation to any communication channel of the CubeSat standard. As an example, FEM prototype was instantiated to I 2 C communication channel to support NanosatC-BR2 testing. NanosatC-BR2 is a Cubesat based scientific mission, under development and integration at Brazilian Institute for Space Research (INPE), which uses I 2 C communication channel for its payloads interactions with the On-Board Data Handling computer subsystem (OBC). FEM prototype was used to support OBC integration testing with each payload subsystem at MIL scenario aiming at anticipating the robustness requirement verification on the development lifecycle. Moreover, the FEM prototype was also validated at HIL scenario using Test Cases automatically generated. Results of these two scenarios executions are reported demonstrating in a case study the effectiveness of FEM framework in detecting the lack or noncompliance of robustness requirements by the interoperated subsystems under testing.
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4. Condições de acesso e uso
Idiomaen
Arquivo Alvobatista_towards.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Política de Arquivamentodenypublisher denyfinaldraft24
Permissão de Leituradeny from all and allow from 150.163
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3EUJHT5
8JMKD3MGPCW/3F35BSP
Lista de Itens Citandosid.inpe.br/bibdigital/2013/10.14.22.20 1
sid.inpe.br/bibdigital/2013/10.05.15.23 1
DivulgaçãoWEBSCI; PORTALCAPES; COMPENDEX.
Acervo Hospedeirourlib.net/www/2017/11.22.19.04
6. Notas
Campos Vaziosalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Controle da descrição
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