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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/449MCUE
Repositorysid.inpe.br/mtc-m21c/2021/03.04.16.41   (restricted access)
Last Update2021:03.04.16.41.44 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21c/2021/03.04.16.41.44
Metadata Last Update2022:04.03.19.24.30 (UTC) administrator
DOI10.1140/epjp/s13360-021-01151-2
ISSN2190-5444
Citation KeyAlmeidaJúniorJohnLeakMort:2021:Fa2iNo
TitleFast 2-impulse non-Keplerian orbit transfer using the Theory of Functional Connections
Year2021
MonthFeb.
Access Date2025, June 02
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size5123 KiB
2. Context
Author1 Almeida Júnior, Allan Kardec de
2 Johnston, Hunter
3 Leake, Carl
4 Mortari, Daniele
Group1 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Texas A&M University
3 Texas A&M University
4 Texas A&M University
Author e-Mail Address1 allan.junior@inpe.br
2 hunterjohnston@tamu.edu
3 leakec@tamu.edu
4 mortari@tamu.edu
JournalEuropean Physical Journal Plus
Volume136
Number2
Pagese223
History (UTC)2021-03-04 16:42:26 :: simone -> administrator :: 2021
2022-04-03 19:24:30 :: administrator -> simone :: 2021
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractThis study applies a new approach, the Theory of Functional Connections (TFC), to solve the two-point boundary-value problem (TPBVP) in non-Keplerian orbit transfer. The perturbations considered are drag, solar radiation pressure, higher-order gravitational potential harmonic terms, and multiple bodies. The proposed approach is applied to Earth-to-Moon transfers and obtains exact boundary condition satisfaction and with very fast convergence. Thanks to this highly efficient approach, perturbed pork-chop plots of Earth-to-Moon transfers are generated, and individual analyses on the transfers parameters are easily done at low computational costs. The minimum fuel analysis is provided in terms of the time of flight, thrust application points, and relative geometry of the Moon and Sun. The transfer costs obtained are in agreement with the literatures best solutions and in some cases are even slightly better.
AreaETES
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4. Conditions of access and use
Languageen
Target Filealmeida_fast.pdf
User Groupsimone
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/46KTFK8
DisseminationWEBSCI; SCOPUS.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
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