Área de identificação | |
Tipo de Referência | Journal Article |
Site | mtc-m21b.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W34P/3MA6MP2 |
Repositório | sid.inpe.br/mtc-m21b/2016/08.19.18.00 (acesso restrito) |
Última Atualização | 2016:08.19.18.01.07 simone |
Metadados | sid.inpe.br/mtc-m21b/2016/08.19.18.00.27 |
Última Atualização dos Metadados | 2021:02.11.20.56.38 administrator |
DOI | 10.1016/j.ymssp.2016.02.026 |
ISSN | 0888-3270 |
Chave de Citação | Mainenti-LopesSouzSous:2016:CoStCo |
Título | A comparative study between control strategies for a solar sailcraft in an Earth–Mars transfer  |
Ano | 2016 |
Mês | Oct. |
Data de Acesso | 08 mar. 2021 |
Tipo de Trabalho | journal article |
Número de Arquivos | 1 |
Tamanho | 913 KiB |
Área de contextualização | |
Autor | 1 Mainenti-Lopes, I. 2 Souza, Luiz Carlos Gadelha de 3 Sousa, Fabiano Luis de |
Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JHN3 3 8JMKD3MGP5W/3C9JH3H |
Grupo | 1 2 DMC-ETE-INPE-MCTI-GOV-BR 3 DSE-ETE-INPE-MCTI-GOV-BR |
Afiliação | 1 Universidade de Brasília (UnB) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) |
Endereço de e-Mail do Autor | 1 rogimainemti@gmail.com 2 gadelha@dem.inpe.br 3 fabiano.sousa@inpe.br |
Revista | Mechanical Systems and Signal Processing |
Volume | 79 |
Páginas | 289-296 |
Tipo Secundário | PRE PI |
Nota Secundária | A1_ENGENHARIAS_III A1_ENGENHARIAS_I A2_ENGENHARIAS_IV B1_MATERIAIS B1_ENGENHARIAS_II B2_ASTRONOMIA_/_FÍSICA |
Histórico | 2016-08-19 18:01:07 :: simone -> administrator :: 2016 2021-02-11 20:56:38 :: administrator -> simone :: 2016 |
Área de conteúdo e estrutura | |
É a matriz ou uma cópia? | é a matriz |
Estágio do Conteúdo | concluido |
Transferível | 1 |
Tipo do Conteudo | External Contribution |
Tipo de Versão | publisher |
Palavras-Chave | Solar sailcraft, Trajectory optimization, Evolutionary algorithm, Generalized extremal optimization. |
Resumo | The 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. |
Area | ETES |
Arranjo | |
Conteúdo da Pasta source | não têm arquivos |
Conteúdo da Pasta agreement | |
Área de condições de acesso e uso | |
Idioma | en |
Arquivo Alvo | mainenti_a comparative.pdf |
Grupo de Usuários | simone |
Grupo de Leitores | administrator simone |
Visibilidade | shown |
Permissão de Leitura | deny from all and allow from 150.163 |
Permissão de Atualização | não transferida |
Área de fontes relacionadas | |
Repositório Espelho | urlib.net/www/2011/03.29.20.55 |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/446AF4B 8JMKD3MGPCW/446AUSL |
Acervo Hospedeiro | sid.inpe.br/mtc-m21b/2013/09.26.14.25.20 |
Área de notas | |
Campos Vazios | alternatejournal 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 secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url |
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