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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Sitemtc-m16b.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositóriosid.inpe.br/mtc-m17@80/2006/12.11.16.12
Última Atualização2007:01.10.18.34.30 (UTC) administrator
Repositório de Metadadossid.inpe.br/mtc-m17@80/2006/12.11.16.12.25
Última Atualização dos Metadados2021:02.11.18.16.55 (UTC) administrator
Chave SecundáriaINPE--PRE/
Chave de CitaçãoMachuyPradStuc:2006:NuStGr
TítuloNumerical study of the gravitational capture in the bicircular four-body problem
Ano2006
Data de Acesso29 abr. 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho109 KiB
2. Contextualização
Autor1 Machuy, Alexandre
2 Prado, Antonio Fernando Bertachini de Almeida
3 Stuchi, Teresinha
Identificador de Curriculo1
2 8JMKD3MGP5W/3C9JGJA
Grupo1
2 DMC-INPE-MCT-BR
Afiliação1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Nome do EventoMathematical Problems in Engineering and Aerospace Sciences, 6.
Localização do EventoBudapest, Hungria
Data21-23 June
Histórico (UTC)2007-01-10 18:34:30 :: vinicius -> administrator ::
2012-10-22 21:03:15 :: administrator -> vinicius :: 2006
2013-02-20 16:29:37 :: vinicius -> administrator :: 2006
2021-02-11 18:16:55 :: administrator -> marciana :: 2006
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
ResumoA gravitational capture occurs when a spacecraft (or any particle with negligible mass) change from a hyperbolic orbit with a small positive energy around a celestial body into an elliptic orbit with a small negative energy without the use of any propulsive system. The force responsible for this modification in the orbit of the spacecraft is the gravitational force of the third and the fourth bodies involved in the dynamics. In this way, those forces are used as a zero cost control, equivalent to a continuous thrust applied in the spacecraft. One of the most important applications of this property is the construction of trajectories to the Moon. The concept of gravitational capture is used together with the basic ideas of the gravity-assisted maneuver and the bi-elliptic transfer orbit to generate a trajectory that requires a fuel consumption smaller than the one required by the Hohmann transfer. The objective of the present paper is to study the energy required for the ballistic gravitational capture in a dynamical model that has the presence of four bodies. In particular, the Earth-Moon-Sun-Spacecraft system is considered.
ÁreaETES
Arranjourlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Numerical study of...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
4. Condições de acesso e uso
URL dos dadoshttp://urlib.net/ibi/sid.inpe.br/mtc-m17@80/2006/12.11.16.12
URL dos dados zipadoshttp://urlib.net/zip/sid.inpe.br/mtc-m17@80/2006/12.11.16.12
Idiomaen
Arquivo Alvoicnpaaalex.pdf
Grupo de Usuáriosadministrator
vinicius
Visibilidadeshown
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
Lista de Itens Citandosid.inpe.br/mtc-m21/2012/07.13.14.40.20 1
sid.inpe.br/bibdigital/2021/02.11.18.06 1
Acervo Hospedeirolcp.inpe.br/ignes/2004/02.12.18.39
cptec.inpe.br/walmeida/2003/04.25.17.12
6. Notas
Campos Vaziosarchivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination documentstage doi e-mailaddress edition editor electronicmailaddress format identifier isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume
7. Controle da descrição
e-Mail (login)marciana
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