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1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Sitemtc-m21b.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34P/3MA6MP2
Repositóriosid.inpe.br/mtc-m21b/2016/08.19.18.00   (acesso restrito)
Última Atualização2016:08.19.18.01.07 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21b/2016/08.19.18.00.27
Última Atualização dos Metadados2021:02.11.20.56.38 (UTC) administrator
DOI10.1016/j.ymssp.2016.02.026
ISSN0888-3270
Chave de CitaçãoMainenti-LopesSouzSous:2016:CoStCo
TítuloA comparative study between control strategies for a solar sailcraft in an Earth–Mars transfer
Ano2016
MêsOct.
Data de Acesso28 abr. 2024
Tipo de Trabalhojournal article
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho913 KiB
2. Contextualização
Autor1 Mainenti-Lopes, I.
2 Souza, Luiz Carlos Gadelha de
3 Sousa, Fabiano Luis de
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JHN3
3 8JMKD3MGP5W/3C9JH3H
Grupo1
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DSE-ETE-INPE-MCTI-GOV-BR
Afiliação1 Universidade de Brasília (UnB)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 rogimainemti@gmail.com
2 gadelha@dem.inpe.br
3 fabiano.sousa@inpe.br
RevistaMechanical Systems and Signal Processing
Volume79
Páginas289-296
Nota SecundáriaA1_ENGENHARIAS_III A1_ENGENHARIAS_I A2_ENGENHARIAS_IV B1_MATERIAIS B1_ENGENHARIAS_II B2_ASTRONOMIA_/_FÍSICA
Histórico (UTC)2016-08-19 18:01:07 :: simone -> administrator :: 2016
2021-02-11 20:56:38 :: administrator -> simone :: 2016
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-ChaveSolar sailcraft
Trajectory optimization
Evolutionary algorithm
Generalized extremal optimization
ResumoThe goal of this work was a comparative study of solar sail trajectory optimization using different control strategies. Solar sailcraft is propulsion system with great interest in space engineering, since it uses solar radiation to propulsion. So there is no need for propellant to be used, thus it can remains active throughout the entire transfer maneuver. This type of propulsion system opens the possibility to reduce the cost of exploration missions in the solar system. In its simplest configuration, a Flat Solar Sail (FSS) consists of a large and thin structure generally composed by a film fixed to flexible rods. The performance of these vehicles depends largely on the sails attitude relative to the Sun. Using a FSS as propulsion, an"Earth-Mars transfer optimization problem was tackled by the algorithms GEO(real1) and GEO(real2) (Generalized Extremal Optimization with real codification). Those algorithms are Evolutionary Algorithms (AE) based on the theory of Self-Organized Criticality. They were used to optimize the FSS attitude angle so it could reach Mars orbit in minimum time. It was considered that the FSS could perform up to ten attitude maneuvers during orbital transfer. Moreover, the time between maneuvers can be different. So, the algorithms had to optimize an objective function with 20 design variables. The results obtained in this work were compared with previously results that considered constant values of time between maneuvers.
ÁreaETES
Arranjo 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A comparative study...
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Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreement
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4. Condições de acesso e uso
Idiomaen
Arquivo Alvomainenti_a comparative.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Permissão de Leituradeny from all and allow from 150.163
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Repositório Espelhourlib.net/www/2011/03.29.20.55
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
8JMKD3MGPCW/446AUSL
Lista de Itens Citandosid.inpe.br/mtc-m21/2012/07.13.14.45.51 3
sid.inpe.br/bibdigital/2021/02.11.18.06 2
sid.inpe.br/bibdigital/2021/02.11.20.54 2
Acervo Hospedeirosid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notas
Campos Vaziosalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination e-mailaddress format isbn label lineage mark nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Controle da descrição
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