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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Siteplutao.sid.inpe.br (namespace prefix: upn:33M4QT8)
Identificador8JMKD3MGP3W/3FCL3B4
Repositóriosid.inpe.br/plutao/2013/12.12.15.12.38
Última Atualização2015:03.10.19.19.02 (UTC) administrator
Repositório de Metadadossid.inpe.br/plutao/2013/12.12.15.12.39
Última Atualização dos Metadados2021:02.11.18.16.24 (UTC) administrator
Rótulolattes: 7752228013890691 1 SilvaKugaGarcZana:2013:AtDeGy
Chave de CitaçãoSilvaKugaGarcZana:2013:AtDeGy
TítuloAttitude Determination and Gyro Calibration for CBERS-2 Satellite
Ano2013
Data de Acesso11 nov. 2026
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho670 KiB
2. Contextualização
Autor1 Silva, William Reis
2 Kuga, Helio Koiti
3 Garcia, Roberta Veloso
4 Zanardi, Maria Cecilia França de Paula Santos
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JHC9
Grupo1 CMC-ETES-SPG-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)
4 Universidade Estadual Paulista (UNESP)
Endereço de e-Mail do Autor1 reis.william@gmail.com
2 helio.kuga@inpe.br
3 rvelosogarcia@yahoo.com.br
4 cecilia@feg.unesp.br
Endereço de e-Mailreis.william@gmail.com
Nome do EventoInternational Conference on Vibration Problems, 11 (ICOVP).
Localização do EventoLisboa
Data2013
Título do LivroProceedings
Tipo TerciárioPaper
Acervo Hospedeirodpi.inpe.br/plutao@80/2008/08.19.15.01 upn:33M4QT8
Histórico (UTC)2013-12-12 17:25:32 :: lattes -> administrator :: 2013
2021-02-11 18:16:24 :: administrator -> marcelo.pazos@inpe.br :: 2013
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-ChaveAttitude determination
Gyro calibration
Nonlinear least-squares
ResumoThis work is applied to the dynamics of rotational motion of artificial satellites, that is, its orientation (attitude) with respect to an inertial reference system. The attitude determination involves approaches of nonlinear estimation techniques, which knowledge is essential to the safety and control of the satellite and payload. Here one focuses on determining the attitude of a real satellite: CBERS-2 (China Brazil Earth Resources Satellite). This satellite was launched in 2003 and were controlled and operated in turns by China (Xian Control Center) and Brazil (Satellite Control Center). Its orbit is near polar sun-synchronous with an altitude of 778km, crossing Equator at 10:30am in descending direction, frozen perigee at 90 degrees, and providing global coverage of the world every 26 days. The attitude dynamical model is described by nonlinear equations involving the Euler angles. The attitude sensors available are two DSS (Digital Sun Sensor), two IRES (Infra-Red Earth Sensor), and one triad of mechanical gyros. The two IRES give direct measurements of roll and pitch angles with a certain level of error. The two DSS are nonlinear functions of roll, pitch, and yaw attitude angles. The gyros furnish the angular measurements in the body frame reference system. Gyros are very important sensors, as they provide direct incremental angles or angular velocities. They can sense instantaneous variations of nominal velocities. An important feature is that it allows the replacement of complex models (different torques acting on the space environment) by using their measurements to turn the dynamical equations into simple kinematic equations. However gyros present several sources of error of which the drift is the most troublesome. Such drifts yield along time an accumulation of errors which must be accounted for in the attitude determination process. Herein one proposes to estimate the attitude and the drift of the gyros using the Least Squares Method. Results show that one can reach accuracies in attitude determination within the prescribed requirements, besides providing estimates of the gyro drifts which can be further used to enhance the gyro error model.
ÁreaETES
ArranjoAttitude Determination and...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
4. Condições de acesso e uso
URI dos dadosupn:33M4QT8:8JMKD3MGP3W/3FCL3B4
URL dos dadoshttp://plutao.sid.inpe.br/ibi/8JMKD3MGP3W/3FCL3B4
URL dos dados zipadoshttp://plutao.sid.inpe.br/zip/8JMKD3MGP3W/3FCL3B4
Idiomaen
Arquivo AlvoSilva_attitude.pdf
Grupo de Usuárioslattes
marcelo.pazos@inpe.br
Grupo de Leitoresadministrator
marcelo.pazos@inpe.br
Visibilidadeshown
Permissão de Leituraallow from all
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Repositório Espelhoiconet.com.br/banon/2006/11.26.21.31
Unidades Imediatamente Superiores8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
Lista de Itens Citandosid.inpe.br/bibdigital/2021/02.11.18.06 - 73
sid.inpe.br/bibdigital/2013/10.14.00.13 - 69
sid.inpe.br/mtc-m21/2012/07.13.14.49.46 - 21
sid.inpe.br/mtc-m21/2012/06.05.15.34.41 - 5
dpi.inpe.br/plutao@80/2008/08.19.15.01.21 - 4
sid.inpe.br/bibdigital@80/2006/04.07.15.50.13 - 4
6. Notas
Campos Vaziosarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor format isbn issn lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject tertiarymark type url volume
7. Controle da descrição
e-Mail (login)marcelo.pazos@inpe.br
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