1. Identificação | |
Tipo de Referência | Capítulo de Livro (Book Section) |
Site | mtc-m21c.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W34R/3SMUC5H |
Repositório | sid.inpe.br/mtc-m21c/2019/02.08.17.13 (acesso restrito) |
Última Atualização | 2019:02.08.17.13.10 (UTC) simone |
Repositório de Metadados | sid.inpe.br/mtc-m21c/2019/02.08.17.13.10 |
Última Atualização dos Metadados | 2020:01.06.11.42.09 (UTC) administrator |
Chave Secundária | INPE--/ |
DOI | 10.1007/978-3-319-99268-6_38 |
Chave de Citação | RomeroSouz:2019:SaCoSy |
Título | Satellite controller system based on reaction wheels using the State-Dependent Riccati Equation (SDRE) on Java |
Ano | 2019 |
Data de Acesso | 25 abr. 2024 |
Tipo Secundário | PRE LI |
Número de Arquivos | 1 |
Tamanho | 1492 KiB |
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2. Contextualização | |
Autor | 1 Romero, Alessandro Gerlinger 2 Souza, Luiz Carlos Gadelha de |
Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JHN3 |
Grupo | 1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR |
Afiliação | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Universidade Federal do ABC (UFABC) |
Endereço de e-Mail do Autor | 1 romgerale@yahoo.com.br 2 luiz.gadelha@ufabc.edu.br |
Editor | Cavalca, Katia Lucchesi Weber, Hans Ingo |
Título do Livro | Proceedings of the 10th International Conference on Rotor Dynamics - IFToMM |
Editora (Publisher) | Springer |
Páginas | 547-561 |
Histórico (UTC) | 2019-02-08 17:13:36 :: simone -> administrator :: 2019 2020-01-06 11:42:09 :: administrator -> simone :: 2019 |
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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 |
Tipo de Versão | publisher |
Palavras-Chave | Nonlinear control · SDRE · Satellite · Attitude Reaction wheels |
Resumo | Complex space missions involving large angle maneuvers and fast attitude control require nonlinear control methods to design the Satellite Controller System (SCS) in order to satisfy robustness and performance requirements. One candidate method for a nonlinear SCS control law is the State-Dependent Riccati Equation (SDRE). SDRE provides an effective algorithm for synthesizing nonlinear feedback control by allowing nonlinearities in the system states while offering great design flexibility through state-dependent weighting matrices. In that context, analysis by simulation of nonlinear control methods can save money and time. Although, commercial 3D simulators exist that can accommodate various satellites components including the controllers, in this paper, we present a 3D simulator and the investigation of a SDRE control law performance by simulations. The simulator is implemented based on Java and related open-source software libraries (Hipparchus - linear algebra library, and Orekit - flight dynamics library), therefore, it can run in a variety of platforms and it has low cost. These open-source libraries were extended in order to solve the optimization problem that is the cornerstone of the SDRE method, a major contribution of the simulator. The simulator is evaluated taking into account a typical mission of the Brazilian National Institute for Space Research (INPE), in which the SCS must stabilize a satellite in three-axis using reaction wheels so that the optical payload can point to the desired target. Two SCS control laws (a linear and a SDRE based) were simulated for an attitude maneuver in the launch and early orbit phase (LEOP), the upside-down maneuver. The results of simulations shown that SDRE-based controller provides better performance. |
Área | ETES |
Arranjo | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Satellite controller system... |
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 | |
Idioma | en |
Arquivo Alvo | romero_satelllite.pdf |
Grupo de Usuários | simone |
Grupo de Leitores | administrator simone |
Visibilidade | shown |
Permissão de Leitura | deny from all |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/3F2UALS |
Lista de Itens Citando | sid.inpe.br/mtc-m21/2012/07.13.14.54.10 5 |
Divulgação | BNDEPOSITOLEGAL |
Acervo Hospedeiro | urlib.net/www/2017/11.22.19.04 |
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6. Notas | |
Campos Vazios | archivingpolicy archivist callnumber city copyholder copyright creatorhistory descriptionlevel e-mailaddress edition format isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url volume |
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7. Controle da descrição | |
e-Mail (login) | simone |
atualizar | |
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