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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Sitemtc-m21b.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34P/3J9R4EP
Repositóriosid.inpe.br/mtc-m21b/2015/04.07.13.20
Última Atualização2015:04.07.13.22.42 (UTC) administrator
Repositório de Metadadossid.inpe.br/mtc-m21b/2015/04.07.13.20.59
Última Atualização dos Metadados2021:02.11.18.19.45 (UTC) administrator
Chave SecundáriaINPE--PRE/
Chave de CitaçãoOliveiraKugaCarr:2015:AiBePl
TítuloAir bearing platforms for simulation of spacecraft attitude control systems
Ano2015
Data de Acesso02 maio 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho1919 KiB
2. Contextualização
Autor1 Oliveira, Alexandre Macedo de
2 Kuga, Hélio Koiti
3 Carrara, Valdemir
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JHC9
3 8JMKD3MGP5W/3C9JJAN
Grupo1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DMC-ETE-INPE-MCTI-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 alexandre.oliveira@inpe.br
2 helio.kuga@inpe.br
3 valdemir.carrara@inpe.br
EditorSteffen Junior, V.
Rade, D. A.
Bessa, W. M.
Nome do EventoInternational Symposium on Dynamic Problems of Mechanics, 17.
Localização do EventoNatal, RN
Data22-27 Feb.
Editora (Publisher)ABCM
Título do LivroProceedings
Histórico (UTC)2015-04-07 13:20:59 :: simone -> administrator ::
2021-02-11 18:19:45 :: administrator -> simone :: 2015
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Tipo de Versãofinaldraft
Palavras-Chaveair bearing
attitude control
satellite simulator
Kalman filter
inertial systems
ResumoThis paper presents the development of two different air bearing tables, which can simulate attitude control systems for satellites with hardware-in-the-loop dynamics and control. Both systems are based on gas-bearing platforms in which several sensors and actuators were fixed. The first platform has a MEMS inertial sensor, and the second platform has several sensors and actuators that are engineering models similar to those usually employed in satellites. A PC/104 computer commands the first platform, which is responsible for driving 8 cold gas thrusters. On the other hand, the second platform is based on a Renesas 32 bits processor, which is responsible for three different subsystems: power supply, data handling and attitude control. The actuators in this case are reaction wheels and magnetic torque coils. The most important process for the correct operation of the simulators is to ensure accurate balancing of both platforms, because a difference between the center of gravity of the platform and the center of rotation of the bearing support may generate higher torques than those normally encountered in the space environment, invalidating the main feature of the simulator. Therefore, we use non-linear filtering to obtain the platforms mass properties, including the center of gravity position. Finally, we validate the mass properties by implementing two simple attitude stabilization controllers. Considerations on the nature of the friction of the two platforms will also be made in the end of this paper.
ÁreaETES
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4. Condições de acesso e uso
URL dos dadoshttp://urlib.net/ibi/8JMKD3MGP3W34P/3J9R4EP
URL dos dados zipadoshttp://urlib.net/zip/8JMKD3MGP3W34P/3J9R4EP
Idiomaen
Arquivo Alvooliveira_air.PDF
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Permissão de Leituraallow from all
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Vinculação8JMKD3MGP5W34M/3GK4L3P
Repositório Espelhourlib.net/www/2011/03.29.20.55
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
Lista de Itens Citandosid.inpe.br/mtc-m21/2012/07.13.14.49.46 1
sid.inpe.br/mtc-m21/2012/07.13.15.01.14 1
sid.inpe.br/mtc-m21b/2013/09.26.14.25.22 1
Acervo Hospedeirosid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notas
Campos Vaziosarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition format isbn issn label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarytype type url volume
7. Controle da descrição
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