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Metadados

1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Sitemtc-m16d.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP7W/3EGJFCL
Repositóriosid.inpe.br/mtc-m19/2013/07.23.19.24
Última Atualização2013:07.25.14.35.00 (UTC) administrator
Repositório de Metadadossid.inpe.br/mtc-m19/2013/07.23.19.24.26
Última Atualização dos Metadados2021:02.11.18.10.34 (UTC) administrator
DOI10.1155/2013/318072
ISSN2314-4904
2314-4912
Chave de CitaçãoSouzaAren:2013:DeSaAt
TítuloDesign of satellite attitude control algorithm based on the SDRE method using gas jets and reaction wheels
Ano2013
Data de Acesso03 maio 2024
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho3150 KiB
2. Contextualização
Autor1 Souza, Luiz Carlos Gadelha de
2 Arena, Victor Massad Ruiz
Identificador de Curriculo1 8JMKD3MGP5W/3C9JHN3
Grupo1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 gadelha@dem.inpe.br
Endereço de e-Mailmarcelo.pazos@inpe.br
RevistaJournal of Engineering
Volume2013
Páginas318072
Histórico (UTC)2013-07-23 19:24:26 :: marcelo.pazos@sid.inpe.br -> administrator ::
2021-02-11 18:10:34 :: 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-Chavesatellite attitude control algorithm
SDRE method
gas jets
reaction wheel torque
space mission cost
angle maneuver
LQR linear controller
SDRE filter
DMC 3D satellite simulator
state-dependent Riccati equation
plant nonlinearities
system noise
angular velocity reduction
switching control algorithm
minimum system energy
ResumoAn experimental attitude control algorithm design using prototypes can minimize space mission costs by reducing the number of errors transmitted to the next phase of the project. The Space Mechanics and Control Division (DMC) of INPE is constructing a 3D simulator to supply the conditions for implementing and testing satellite control hardware and software. Satellite large angle maneuver makes the plant highly nonlinear and if the parameters of the system are not well determined, the plant can also present some level of uncertainty. As a result, controller designed by a linear control technique can have its performance and robustness degraded. In this paper the standard LQR linear controller and the SDRE controller associated with an SDRE filter are applied to design a controller for a nonlinear plant. The plant is similar to the DMC 3D satellite simulator where the unstructured uncertainties of the system are represented by process and measurements noise. In the sequel the State-Dependent Riccati Equation (SDRE) method is used to design and test an attitude control algorithm based on gas jets and reaction wheel torques to perform large angle maneuver in three axes. The SDRE controller design takes into account the effects of the plant nonlinearities and system noise which represents uncertainty. The SDRE controller performance and robustness are tested during the transition phase from angular velocity reductions to normal mode of operation with stringent pointing accuracy using a switching control algorithm based on minimum system energy. This work serves to validate the numerical simulator model and to verify the functionality of the control algorithm designed by the SDRE method.
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4. Condições de acesso e uso
URL dos dadoshttp://urlib.net/ibi/8JMKD3MGP7W/3EGJFCL
URL dos dados zipadoshttp://urlib.net/zip/8JMKD3MGP7W/3EGJFCL
Idiomaen
Arquivo Alvo318072.pdf
Grupo de Usuáriosmarcelo.pazos@inpe.br
Grupo de Leitoresadministrator
marcelo.pazos@inpe.br
Visibilidadeshown
Política de Arquivamentoallowpublisher allowfinaldraft
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Repositório Espelhoiconet.com.br/banon/2006/11.26.21.31
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
Lista de Itens Citandosid.inpe.br/bibdigital/2021/02.11.18.06 2
sid.inpe.br/mtc-m21/2012/07.13.14.54.10 1
URL (dados não confiáveis)http://dx.doi.org/10.1155/2013/318072
DivulgaçãoPORTALCAPES
Acervo Hospedeirosid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notas
Campos Vaziosalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn label lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Controle da descrição
e-Mail (login)marcelo.pazos@inpe.br
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