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/43MHJ9L |
Repositório | sid.inpe.br/mtc-m21c/2020/12.01.13.33 (acesso restrito) |
Última Atualização | 2020:12.01.13.33.17 (UTC) simone |
Repositório de Metadados | sid.inpe.br/mtc-m21c/2020/12.01.13.33.17 |
Última Atualização dos Metadados | 2022:01.04.01.35.39 (UTC) administrator |
DOI | 10.1007/s11071-020-05992-x |
ISSN | 0924-090X |
Chave de Citação | FerreiraMoraPradWint:2020:MaStTe |
Título | A mathematical study of the tethered slingshot maneuver using the elliptic restricted problem |
Ano | 2020 |
Data de Acesso | 09 maio 2024 |
Tipo de Trabalho | journal article |
Tipo Secundário | PRE PI |
Número de Arquivos | 1 |
Tamanho | 3348 KiB |
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2. Contextualização | |
Autor | 1 Ferreira, Alessandra Ferraz da Silva 2 Moraes, Rodolpho Vilhena de 3 Prado, Antonio Fernando Bertachini de Almeida 4 Winter, Othon C. |
Identificador de Curriculo | 1 2 3 8JMKD3MGP5W/3C9JGJA |
ORCID | 1 0000-0002-6162-9078 2 0000-0003-1289-8332 3 0000-0002-7966-3231 4 0000-0002-4901-3289 |
Grupo | 1 2 3 DIDMC-CGETE-INPE-MCTIC-GOV-BR |
Afiliação | 1 Universidade Estadual Paulista (UNESP) 2 Universidade Estadual Paulista (UNESP) 3 Instituto Nacional de Pesquisas Espaciais (INPE) 4 Universidade Estadual Paulista (UNESP) |
Endereço de e-Mail do Autor | 1 aleferrazsilva@hotmail.com 2 rodolpho.vilhena@gmail.com 3 antonio.prado@inpe.br 4 othon.winter@unesp.br |
Revista | Nonlinear Dynamics |
Volume | 102 |
Páginas | 1585-1609 |
Nota Secundária | A2_INTERDISCIPLINAR A2_ENGENHARIAS_III A2_ENGENHARIAS_I B1_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA B1_ENGENHARIAS_IV B1_ENGENHARIAS_II B3_ASTRONOMIA_/_FÍSICA |
Histórico (UTC) | 2020-12-01 13:33:17 :: simone -> administrator :: 2020-12-01 13:33:18 :: administrator -> simone :: 2020 2020-12-14 13:40:05 :: simone -> administrator :: 2020 2022-01-04 01:35:39 :: administrator -> simone :: 2020 |
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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 | Astrodynamics Tethered slingshot maneuver Tether Spacecraft Orbital maneuvers Energy variation |
Resumo | The main objective of the present paper is to find the modifications that a tethered slingshot maneuver (TSSM) can make in the orbit of a spacecraft, both in terms of energy and inclination. The TSSM is a maneuver where a tether fixed in a celestial body, like a moon or an asteroid, makes a rotation in the velocity vector of a spacecraft to modify its orbit. In particular, the present paper concentrates in showing the potential savings in fuel consumption for orbital maneuvers that use this technique in an elliptic system of primaries, which gives advantages over the circular problem. To make this study more complete, analytical approximations are derived to provide a general view of the behavior of the maneuver in terms of variations of energy and inclination as a function of different conditions for the geometry, length, and location of the tether. Among the main results, it is showed the best location to place the tether and the best moment and duration to perform the maneuver, as a function of the parameters involved, like the orbits of the primaries, the incoming velocity of the spacecraft, etc. The solutions are shown in maps giving the variations of energy and inclination for different locations of this device and assuming different incoming orbits for the spacecraft. Regions that maximize those variations are indicated. Based on those results, it is possible to find the best solution for several particular problems. The results show that this maneuver has a large potential to be explored, helping a spacecraft to make journeys to the exterior planets and out of the Solar System. Those results are arguments in favor of developing efforts to solve the technological problems involved in real applications of this technique. The main advantage of the proposed technique is the energy gain given by the maneuver, in particular when using the higher velocity of the asteroid, at the periapsis of its orbit around the Sun. The main disadvantages are the technical challenges involved in the implementation of the maneuver and the fact that to get maximum benefits, there are time restrictions to apply the maneuver, because the asteroid must be passing by its periapsis. |
Área | ETES |
Arranjo | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A mathematical study... |
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 | Ferreira2020_Article_AMathematicalStudyOfTheTethere.pdf |
Grupo de Usuários | simone |
Grupo de Leitores | administrator simone |
Visibilidade | shown |
Política de Arquivamento | denypublisher denyfinaldraft12 |
Permissão de Leitura | deny from all and allow from 150.163 |
Permissão de Atualização | não transferida |
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5. Fontes relacionadas | |
Unidades Imediatamente Superiores | 8JMKD3MGPCW/446AF4B |
Lista de Itens Citando | sid.inpe.br/bibdigital/2021/02.11.18.06 4 sid.inpe.br/mtc-m21/2012/07.13.14.40.20 1 |
Divulgação | WEBSCI; PORTALCAPES. |
Acervo Hospedeiro | urlib.net/www/2017/11.22.19.04 |
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6. Notas | |
Campos Vazios | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository month nextedition notes number parameterlist parentrepositories previousedition previouslowerunit progress project 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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