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1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Sitemarte3.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador6qtX3pFwXQZ3r59YCT/GUPMc
Repositóriosid.inpe.br/iris@1905/2005/07.30.01.50.42   (acesso restrito)
Última Atualização2015:09.09.18.22.32 (UTC) marciana
Repositório de Metadadossid.inpe.br/iris@1905/2005/07.30.01.50.58
Última Atualização dos Metadados2021:02.11.18.13.40 (UTC) administrator
Chave SecundáriaINPE-9207-PRE/4880
ISSN0100-7386
Rótulo10092
Chave de CitaçãoLopesOrlKugGueKon:1994:AtDeBr
TítuloAttitude determination of the brazilian satellite SCD1
Ano1994
Data de Acesso18 maio 2024
Tipo SecundárioPRE PN
Número de Arquivos1
Tamanho656 KiB
2. Contextualização
Autor1 Lopes, Roberto Vieira da Fonseca
2 Orlando, Valcir
3 Kuga, Hélio Koiti
4 Guedes, Ulisses Thadeu
5 Kondapalli, Rama Rao
Grupo1 DMC-INPE-MCT-BR
RevistaRevista Brasileira de Ciências Mecânicas
Volume16
NúmeroSpecial Issue
Páginas11-18
Histórico (UTC)2008-06-09 16:29:03 :: administrator -> banon ::
2010-05-11 15:57:51 :: banon -> administrator ::
2014-09-29 15:13:46 :: administrator -> marciana :: 1994
2015-09-09 18:22:32 :: marciana -> administrator :: 1994
2021-02-11 18:13:40 :: administrator -> marciana :: 1994
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Palavras-ChaveENGENHARIA E TECNOLOGIA ESPACIAL
SPACECRAFT DESIGN
TESTING AND PERFORMANCE
EVIRONMENTAL RESEARCH SATELLITES
SATELLITE ATTITUDE CONTROL
SPACECRAFT PERFORMANCE
SPIN STABILIZATION
APPLICATIONS PROGRAMS (COMPUTERS)
BRAZILIAN SPACE PROGRAM
GROUND SUPPORT SYSTEMS
OPERATIONAL PROBLEMS
PROBLEM SOLVING
SCD 1
Data Collection Satellite
ResumoThis paper describes the main aspects of the attitude determination related to the first Brazilian satellite: the Data Collection Satellite (SCD1). The satellite was developed by the National Institute for Space Research (INPE) as the first of the four scheduled by the program called Complete Brazilian Space Mission (MECB). It is spin-stabilized and was injected in a near-circular orbit, at an altitude of approximately 760 km. The attitude determination is achieved in two phases. In the first one, preliminary attitude is computed from sensors' telemetry data corresponding to passes over the tracking station. In the second one, data encompassing all the preliminary attitudes are processed to fit a dynamic model whose parameters are estimated. This paper aims at describing these procedures, their mathematical development and their evolution along time since the conception of the project. We also describe our first experience of a real satellite attitude determination, main difficulties, problems faced, as well as the solutions sketched at the very last minute. The results obtained are presented and discussed based on the expected performance of the software developed by the INPE's flight dynamics team.
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4. Condições de acesso e uso
Arquivo Alvo1994_lopes.pdf
Grupo de Usuáriosadministrator
banon
marciana
Grupo de Leitoresadministrator
marciana
Visibilidadeshown
Política de Arquivamentodenypublisher denyfinaldraft
Permissão de Leituradeny from all and allow from 150.163
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
DivulgaçãoPORTALCAPES; SCIELO.
Acervo Hospedeirosid.inpe.br/banon/2001/04.03.15.36
6. Notas
NotasInternational Symposium on Spacecraft Ground Control and Flight Dynamics, 7-11 Feb., 1994, São José dos Campos.
Campos Vaziosaffiliation alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress electronicmailaddress format isbn language lineage mark mirrorrepository month nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project resumeid rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype
7. Controle da descrição
e-Mail (login)marciana
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