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Metadados

1. Identificação
Tipo de ReferênciaCapítulo de Livro (Book Section)
Sitemtc-m21c.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34R/3SMUC5H
Repositóriosid.inpe.br/mtc-m21c/2019/02.08.17.13   (acesso restrito)
Última Atualização2019:02.08.17.13.10 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21c/2019/02.08.17.13.10
Última Atualização dos Metadados2020:01.06.11.42.09 (UTC) administrator
Chave SecundáriaINPE--/
DOI10.1007/978-3-319-99268-6_38
Chave de CitaçãoRomeroSouz:2019:SaCoSy
TítuloSatellite controller system based on reaction wheels using the State-Dependent Riccati Equation (SDRE) on Java
Ano2019
Data de Acesso13 maio 2024
Tipo SecundárioPRE LI
Número de Arquivos1
Tamanho1492 KiB
2. Contextualização
Autor1 Romero, Alessandro Gerlinger
2 Souza, Luiz Carlos Gadelha de
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JHN3
Grupo1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Federal do ABC (UFABC)
Endereço de e-Mail do Autor1 romgerale@yahoo.com.br
2 luiz.gadelha@ufabc.edu.br
EditorCavalca, Katia Lucchesi
Weber, Hans Ingo
Título do LivroProceedings of the 10th International Conference on Rotor Dynamics - IFToMM
Editora (Publisher)Springer
Páginas547-561
Histórico (UTC)2019-02-08 17:13:36 :: simone -> administrator :: 2019
2020-01-06 11:42:09 :: 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-ChaveNonlinear control · SDRE · Satellite · Attitude Reaction wheels
ResumoComplex 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.
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4. Condições de acesso e uso
Idiomaen
Arquivo Alvoromero_satelllite.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Permissão de Leituradeny from all
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3F2UALS
Lista de Itens Citandosid.inpe.br/mtc-m21/2012/07.13.14.54.10 5
sid.inpe.br/bibdigital/2013/10.14.00.13 1
DivulgaçãoBNDEPOSITOLEGAL
Acervo Hospedeirourlib.net/www/2017/11.22.19.04
6. Notas
Campos Vaziosarchivingpolicy 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
7. Controle da descrição
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