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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br (namespace prefix: upn:44QHRCS)
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/46HABS8
Repositorysid.inpe.br/mtc-m21d/2022/03.18.12.55   (restricted access)
Last Update2022:03.18.12.55.38 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21d/2022/03.18.12.55.38
Metadata Last Update2023:01.03.16.46.02 (UTC) administrator
DOI10.1038/s41598-022-08046-x
ISSN2045-2322
Citation KeyAlmeidaJúniorPrad:2022:CoThCi
TitleComparisons between the circular restricted three-body and bi-circular four body problems for transfers between the two smaller primaries
Year2022
MonthMar.
Access Date2025, Dec. 07
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size14797 KiB
2. Context
Author1 Almeida Júnior, Allan Kardec de
2 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
ORCID1 0000-0002-9488-4462
2 0000-0002-7966-3231
Group1 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR
2 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 allan.junior@inpe.br
2 antonio.prado@inpe.br
JournalScientific Reports
Volume12
Number1
Pagese4148
Secondary MarkB2_BIODIVERSIDADE B3_ODONTOLOGIA B3_LETRAS_/_LINGUÍSTICA C_CIÊNCIAS_BIOLÓGICAS_III C_BIOTECNOLOGIA C_ASTRONOMIA_/_FÍSICA
Host Collectionurlib.net/www/2021/06.04.03.40 upn:44QHRCS
History (UTC)2022-03-18 12:55:52 :: simone -> administrator :: 2022
2023-01-03 16:46:02 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractImportant properties of the dynamics of a spacecraft can be obtained from the Circular Restricted Three Body Problem and the Bi-Circular Bi-planar Four Body Problem. In this work, both systems are compared under the perspective of the costs involved in a transfer between the smaller primaries. An analytical approach shows several properties of the perturbation due to the gravity of the Sun and the motion of the smaller primaries around it over a spacecraft in the region of interest, like its behavior at and around the barycenter or at any point in a circle around the Sun. The costs involved in transfers between the smaller primaries are numerically evaluated and analyzed using the newly developed Theory of Functional Connections. The results show that the influence of this perturbation over the costs is significant for systems like the Sun-Earth-Moon or Sun-Mars-Phobos. On the other hand, it is also shown that this influence may be negligible for other very different systems, like the Sun-Saturn-Titan or Sun-Ida-Dactyl. Maps of perturbation are drawn in the region of interest, which can be used for mission designers. Finally, a new approach to describe the influence of the Sun over the tides of the smaller primaries is proposed under the Four Body Problem model.
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4. Conditions of access and use
Languageen
Target Filealmeida jr_2022_comparisons.pdf
User Groupsimone
Reader Groupadministrator
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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/2013/10.14.00.13 - 43
sid.inpe.br/bibdigital/2022/04.03.17.52 - 43
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 16
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
6. Notes
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