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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br (namespace prefix: upn:33M4QT8)
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/474NTS5
Repositorysid.inpe.br/plutao/2022/06.15.12.28.51   (restricted access)
Last Update2022:06.20.16.36.08 (UTC) lattes
Metadata Repositorysid.inpe.br/plutao/2022/06.15.12.28.52
Metadata Last Update2023:01.03.16.52.55 (UTC) administrator
DOI10.3390/sym14061132
ISSN2073-8994
Labellattes: 1226006844793712 1 RibeiroMeloPrad:2022:ApTrNe
Citation KeyRibeiroMeloPrad:2022:ApTrNe
TitleTrajectories Derived from Periodic Orbits around the Lagrangian Point L1 and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids
Year2022
Access Date2025, Dec. 08
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size6762 KiB
2. Context
Author1 Ribeiro, Rebeca de Souza
2 Melo, Cristiano F. de
3 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
Group1 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR
2
3 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Federal de Minas Gerais (UFMG)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 rebeca.ribeiro@inpe.br
2 cristiano.fiorilo@demec.ufmg.br
3 antonio.prado@inpe.br
JournalSymmetry
Volume14
Number6
Pages1132
History (UTC)2022-06-15 12:36:55 :: lattes -> administrator :: 2022
2022-06-16 00:01:24 :: administrator -> lattes :: 2022
2022-06-20 16:36:10 :: lattes -> administrator :: 2022
2023-01-03 16:52:55 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordsperiodic orbits
escape trajectories
lunar swing-by
near-earth asteroids
mission analysis
AbstractTo present a set of trajectories derived from the retrograde periodic orbits around the Lagrangian equilibrium point L1 , this paper considers the Circular Restricted Three-body Problem with Earth-Moon masses (CR3BP), the Restricted Bicircular, and Full Four-Body Sun-Earth-Moonspacecraft Problems (BCR4BP and FR4BP, respectively). These periodic orbits are predicted by the dynamics of the CR3BP. To generate the trajectories of this set, first, slightly different increments of velocity (∆Vs) from those needed to generate periodic orbits around L1 are applied to a spacecraft in circular low Earth orbits in the same direction of their motion when the Earth, the spacecraft, and the Moon are aligned in this order. Thus, translunar trajectories derived from the periodic orbits are obtained and they will lead the spacecraft to the vicinity of the Moon. Depending on the values of the |∆Vs|, which are also functions of the relative positioning between the Sun, the Earth, and the Moon, three types of trajectories of interest are found: Collision with the Moon, escape, and geocentric orbits with large semi-major axes. For a well-defined interval of the |∆Vs|, the trajectories accomplish swing-bys with the Moon and obtain energy to escape from the EarthMoon system and reach Near-Earth Asteroids (NEAs) between the orbits of Venus and Mars. This procedure reduces the costs of inserting spacecraft into transfer trajectories to a set of NEAs in terms of the required |∆V| by up to 5% when compared to Lamberts problem, for example. This work also presents analyses of examples of transfers to the NEAs 3361 Orpheus, 99942 Apophis, and 65803 Didymos, from 2025 on.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Trajectories Derived from...
Arrangement 2urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Trajectories Derived from...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filesymmetry-14-01132-v2.pdf
Reader Groupadministrator
lattes
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/46KTFK8
Citing Item Listsid.inpe.br/bibdigital/2022/04.03.17.52 - 31
sid.inpe.br/bibdigital/2013/10.14.00.13 - 25
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 7
DisseminationPORTALCAPES; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
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