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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/485DNLL
Repositorysid.inpe.br/mtc-m21d/2022/12.02.15.39   (restricted access)
Last Update2022:12.02.15.39.02 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2022/12.02.15.39.03
Metadata Last Update2023:01.03.16.46.26 (UTC) administrator
DOI10.1016/j.asr.2022.08.035
ISSN0273-1177
1879-1948
Citation KeySantosSoTeMaAlMePr:2022:OpTrMo
TitleOptimal transfers from Moon to L2 halo orbit of the Earth-Moon system
Year2022
MonthDec.
Access Date2024, May 13
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size1373 KiB
2. Context
Author1 Santos, Leonardo Barbosa Torres dos
2 Sousa Silva, P. A.
3 Terra, M. O
4 Mani, Karthik V.
5 Almeida Júnior, Alan Kardec de
6 Merguizo Sanchez, Diogo
7 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2
3
4
5
6
7 8JMKD3MGP5W/3C9JGJA
Group1 DIMEC-CGCE-INPE-MCTI-GOV-BR
2
3
4
5 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR
6 DIMEC-CGCE-INPE-MCTI-GOV-BR
7 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Estadual Paulista (UNESP)
3 Instituto Tecnológico de Aeronáutica (ITA)
4 GomSpace
5 Instituto Nacional de Pesquisas Espaciais (INPE)
6 Instituto Nacional de Pesquisas Espaciais (INPE)
7 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 leonardobarbosat@hotmail.com
2
3
4
5 fenixcinza@gmail.com
6 sanchezfisica@gmail.com
7 antonio.prado@inpe.br
JournalAdvances in Space Research
Volume70
Number11
Pages3362-3372
Secondary MarkB1_INTERDISCIPLINAR B1_GEOCIÊNCIAS B1_ENGENHARIAS_IV B1_ENGENHARIAS_III B1_BIODIVERSIDADE B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ASTRONOMIA_/_FÍSICA C_CIÊNCIAS_BIOLÓGICAS_I
History (UTC)2022-12-02 15:39:03 :: simone -> administrator ::
2022-12-02 15:39:03 :: administrator -> simone :: 2022
2022-12-02 15:41:20 :: simone -> administrator :: 2022
2023-01-03 16:46:26 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsMission design
Moon to L2 Halo orbit transfer
Optimal transfers
Restricted three-body problem
Stable manifold
AbstractIn this paper, optimal solutions are investigated for a transfer from a parking orbit around the Moon to a halo orbit around L2 of the Earth-Moon system. The transfers are executed by applying a single maneuver and exploiting the stable invariant manifold of the hyperbolic parking solution at arrival. In this regard, an optimization problem is proposed where both the orbital characteristics of a parking solution around the Moon (its Keplerian elements) and the characteristics of a transfer trajectory (guided by the stable manifold of the arrival Halo orbit) are considered as variables. The problem involved in the single maneuver transfer is solved using a nonlinear programming method (NLP), which aims to minimize the cost of ΔV within the framework of the Earth-Moon system using the circular restricted three-body problem. The feasibility of this kind of transfer for a Cubesat is shown in this paper through results with low ΔV combined with suitable times of flight.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Optimal transfers from...
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4. Conditions of access and use
Languageen
Target FileOptimal transfers from Moon to halo orbit of the Earth-Moon system.pdf
User Groupsimone
Reader Groupadministrator
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Visibilityshown
Archiving Policydenypublisher denyfinaldraft24
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 2
sid.inpe.br/bibdigital/2013/10.14.00.13 2
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionurlib.net/www/2021/06.04.03.40
6. Notes
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