1. Identificação | |
Tipo de Referência | Artigo em Revista Científica (Journal Article) |
Site | mtc-m21c.sid.inpe.br |
Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identificador | 8JMKD3MGP3W34R/3SKLFDL |
Repositório | sid.inpe.br/mtc-m21c/2019/01.25.14.54 (acesso restrito) |
Última Atualização | 2019:01.25.14.54.52 (UTC) administrator |
Repositório de Metadados | sid.inpe.br/mtc-m21c/2019/01.25.14.54.52 |
Última Atualização dos Metadados | 2021:07.28.22.52.25 (UTC) administrator |
DOI | 10.1007/s40314-017-0483-4 |
ISSN | 2238-3603 |
Chave de Citação | FerreiraPradWint:2018:PlPoSw |
Título | Planar powered Swing-By maneuvers to brake a spacecraft |
Ano | 2018 |
Mês | Dec. |
Data de Acesso | 02 maio 2024 |
Tipo de Trabalho | journal article |
Tipo Secundário | PRE PI |
Número de Arquivos | 1 |
Tamanho | 2726 KiB |
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2. Contextualização | |
Autor | 1 Ferreira, Alessandra F. S. 2 Prado, Antonio Fernando Bertachini de Almeida 3 Winter, Othon C. |
Identificador de Curriculo | 1 2 8JMKD3MGP5W/3C9JGJA |
Grupo | 1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR 2 DIDMC-CGETE-INPE-MCTIC-GOV-BR |
Afiliação | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Universidade Estadual Paulista (UNESP) |
Endereço de e-Mail do Autor | 1 aleferrazsilva@hotmail.com 2 antonio.prado@inpe.br 3 ocwinter@gmail.com |
Revista | Computational and Applied Mathematics |
Volume | 37 |
Número | Suppl. 1 |
Páginas | 202-219 |
Nota Secundária | B2_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B2_INTERDISCIPLINAR B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ENGENHARIAS_IV |
Histórico (UTC) | 2019-01-25 14:55:15 :: simone -> administrator :: 2018 2021-07-28 22:52:25 :: administrator -> simone :: 2018 |
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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 | Powered Swing-By Close approach Impulsive maneuvers Spacecraft trajectory Energy decrease |
Resumo | The Swing-By maneuver is a technique used in many space mission to modify the trajectory of a spacecraft. The most usual goal is to increase the energy of the spacecraft, but it is also possible to reduce this energy. An important application is to break a spacecraft coming to the Earth using a Swing-By with the moon, which is the example used in the present paper. Other possibilities also exist, such as reducing the velocity of a spacecraft going to the planets Mercury or Venus. The goal is to help a possible capture by the planet, or at least to provide a passage with smaller velocities to allow better observations during the passage. Therefore, the goal of the present paper is to study the energy loss that a spacecraft may have during a powered Swing-By maneuver, which is a maneuver that combines a close approach by a celestial body with the application of an impulsive maneuver. The behavior of the energy variation is analyzed as a function of the parameters related to the pure gravity maneuver: periapsis radius, angle of approach and approach velocity; and the parameters related to the impulsive maneuver: the location of application of the impulse and its direction and magnitude. The maneuver is performed in a system composed by two bodies, such as the Earth-moon system, around the secondary body, and the energy is measured with respect to the primary body of the system. This problem is solved by developing a mathematical algorithm that guides larger efforts in terms of computer simulations. The results show maps of conditions made from the numerical simulations for different points of application and direction of the impulse, where the maneuver is advantageous and how much more energy can be removed from the spacecraft. |
Área | ETES |
Arranjo 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Planar powered Swing-By... |
Arranjo 2 | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Planar powered Swing-By... |
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 | ferreira_planar.pdf |
Grupo de Usuários | simone |
Visibilidade | shown |
Permissão de Leitura | deny from all and allow from 150.163 |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Repositório Espelho | urlib.net/www/2017/11.22.19.04.03 |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/3F2UALS 8JMKD3MGPCW/446AF4B |
Divulgação | WEBSCI; PORTALCAPES; SCOPUS. |
Acervo Hospedeiro | urlib.net/www/2017/11.22.19.04 |
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6. Notas | |
Campos Vazios | alternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url |
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7. Controle da descrição | |
e-Mail (login) | simone |
atualizar | |
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