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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3D53AB5
Repositorydpi.inpe.br/plutao/2012/11.28.14.42.30   (restricted access)
Last Update2013:02.20.12.37.56 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/11.28.14.42.31
Metadata Last Update2018:06.05.00.01.57 (UTC) administrator
Secondary KeyINPE--PRE/
DOI10.1007/s10569-012-9426-y
ISSN0923-2958
Labellattes: 0793627832164040 3 SalazarMeloMacaWint:2012:ThPrLa
Citation KeySalazarMeloMacaWint:2012:ThPrLa
TitleThree-body problem, its Lagrangian points and how to exploit them using an alternative transfer to L4 and L5
Year2012
MonthOct.
Access Date2024, May 19
Secondary TypePRE PI
Number of Files1
Size713 KiB
2. Context
Author1 Salazar, F. J. T.
2 Melo, Cristiano Fiorilo de
3 Macau, Elbert Einstein Nehrer
4 Winter, Othon Cabo
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGUT
Group1 LAC-CTE-INPE-MCTI-GOV-BR
2
3 LAC-CTE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Federal do ABC, Rua Santa Adélia 166, Santo André, SP, 09210-170, Brazil O. C. Winter
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 Univ Estadual Paulista—UNESP, Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá, SP 12516-410, Brazil
Author e-Mail Address1
2
3 elbert@lac.inpe.br
e-Mail Addresselbert@lac.inpe.br
JournalCelestial Mechanics and Dynamical Astronomy
Volume114
Number1-2
Pages201-213
History (UTC)2012-11-28 23:06:23 :: lattes -> administrator :: 2012
2012-11-30 13:52:32 :: administrator -> marciana :: 2012
2012-12-27 15:38:39 :: marciana -> administrator :: 2012
2013-01-20 15:54:27 :: administrator -> marciana :: 2012
2013-02-18 14:23:51 :: marciana -> administrator :: 2012
2013-02-18 14:29:15 :: administrator -> marciana :: 2012
2013-02-20 12:37:56 :: marciana -> banon :: 2012
2013-02-20 12:42:19 :: banon -> administrator :: 2012
2018-06-05 00:01:57 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordsalternative transfers
stable Lagrangian points
L4
L5
three-body problem
trajectories-G
controle de caos
dinamica nao linear
astrodinâmica
dinâmica orbital
AbstractAn alternative transfer strategy to send spacecraft to stable orbits around the Lagrangian equilibrium points L4 and L5 based in trajectories derived from the periodic orbits around L1 is presented in this work. The trajectories derived, called Trajectories G, are described and studied in terms of the initial generation requirements and their energy variations relative to the Earth through the passage by the lunar sphere of influence. Missions for insertion of spacecraft in elliptic orbits around L4 and L5 are analysed considering the restricted three-body problem Earth-Moon-particle and the results are discussed starting from the thrust, time of flight and energy variation relative to the Earth.
AreaCOMP
Arrangementurlib.net > Fonds > Produção anterior à 2021 > LABAC > Three-body problem, its...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filemacaulac.pdf
User Groupadministrator
banon
lattes
marciana
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3ESGTTP
URL (untrusted data)http://link.springer.com/article/10.1007/s10569-012-9426-y?null
DisseminationWEBSCI; PORTALCAPES.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn lineage mark mirrorrepository nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Description control
e-Mail (login)marciana
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