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1. Identity statement
Reference TypeJournal Article
Sitemtc-m16b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZGivnK2Y/NqFP6
Repositorysid.inpe.br/mtc-m17@80/2006/12.11.12.30   (restricted access)
Last Update2006:12.11.12.30.46 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m17@80/2006/12.11.12.30.47
Metadata Last Update2021:02.11.18.11.45 (UTC) administrator
Secondary KeyINPE-14436-PRE/9516
ISSN0100-7386
Citation KeyPrado:2006:AnNuAp
TitleAnalytical and numerical approaches to study the gravitational capture in the four-body Poblem
ProjectTrajetórias Espaciais
Year2006
MonthJuly-Sept.
Access Date2024, Apr. 27
Secondary TypePRE PI
Number of Files1
Size247 KiB
2. Context
AuthorPrado, Antonio Fernando Bertachini de Almeida
Resume Identifier8JMKD3MGP5W/3C9JGJA
GroupDMC-INPE-MCT-BR
AffiliationInstituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Addressprado@dem.inpe.br
JournalJournal of the Brazilian Society of Mechanical Sciences and Engineering
Volume28
Number3
Pages347-353
History (UTC)2007-03-20 12:36:48 :: vinicius -> administrator ::
2008-06-29 02:29:55 :: administrator -> vinicius ::
2011-05-29 09:26:30 :: vinicius -> administrator ::
2012-11-24 01:39:43 :: administrator -> vinicius :: 2006
2013-02-20 16:29:36 :: vinicius -> administrator :: 2006
2021-02-11 18:11:45 :: administrator -> marciana :: 2006
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
astrodinâmica
captura gravitacional
astrodynamics
gravitational capture
celestial mechanics
restricted four-body problem
AbstractThe objective of this paper is to study the problem of gravitational capture in the bicircular restricted four-body problem. A gravitational capture occurs when a massless particle changes its two-body energy around one celestial body from positive to negative without the use of non-gravitational forces. It is mainly studied the effect of the fourth-body included in the dynamics. The Earth-Moon system with the inclusion of the Sun is used for the numerical simulations. The results show the savings obtained in this more realistic model when compared with the more traditional restricted three-body problem model. It is clear that large savings are obtained thanks to the effect of the Sun, if a proper geometry is used for the maneuver.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Analytical and numerical...
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4. Conditions of access and use
Languageen
Target Fileprado-analytical.pdf
User Groupadministrator
vinicius
Visibilityshown
Copy HolderSID/SCD
Archiving Policydenypublisher denyfinaldraft
Read Permissiondeny from all and allow from 150.163
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES.
Host Collectionlcp.inpe.br/ignes/2004/02.12.18.39
cptec.inpe.br/walmeida/2003/04.25.17.12
6. Notes
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7. Description control
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