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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3D537JA
Repositorydpi.inpe.br/plutao/2012/11.28.14.09.17
Last Update2015:03.18.17.21.33 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/11.28.14.09.18
Metadata Last Update2021:02.11.18.16.08 (UTC) administrator
Secondary KeyINPE--PRE/
Labellattes: 7340081273816424 3 FariaVendittiRoccPrad:2012:MuOpIn
Citation KeyFariaVendittiRoccPrad:2012:MuOpIn
TitleMulti-Objective Optimization of Interplanetary Trajectories with Sequential Gravity Assisted Maneuvers
Year2012
Access Date2024, May 15
Secondary TypePRE CN
Number of Files1
Size709 KiB
2. Context
Author1 Faria Venditti, Flaviane Cristine
2 Rocco, Evandro Marconi
3 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
3 8JMKD3MGP5W/3C9JGJA
Group1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 flaviane.venditti@gmail.com
2 evandro@dem.inpe.br
3 prado@dem.inpe.br
e-Mail Addressprado@dem.inpe.br
Conference NameCongresso Nacional de Engenharia Mecânica, 7 (CONEM).
Conference LocationSão Luís
Date2012
PublisherABCM
Volume1
Pages1-10
Book TitleAnais
Tertiary TypePaper
History (UTC)2012-11-28 23:06:21 :: lattes -> marciana :: 2012
2012-12-14 11:06:04 :: marciana -> administrator :: 2012
2021-02-11 18:16:08 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodinâmica
Dinâmica Orbital
Swing-By
AbstractThis work is a study of optimization of interplanetary trajectories using gravity assisted maneuvers on different planets on the same mission. This maneuver consists in using the gravity of a planet to gain or lose energy, velocity and angular momentum, minimizing fuel consumption. The trajectory is divided into three parts, where the first and the last one are inside the sphere of influence of a planet, and the intermediate part is a heliocentric phase. This methodology is called Patched Conics. When the optimization of more than one objective is desired, considering that the objectives are conflicting, a multi-objective method is needed. The optimization problem is solved using a methodology based on the Non Inferiority Criterion (Pareto, 1909) and the Smallest Loss Criterion (Rocco et al. 2003), where all objectives are considered simultaneously, without reducing the problem to the case of optimizing a single objective as occurs in most methods found in literature. For this purpose a sequence of gravity assisted maneuvers on some planets were tested with different combinations of dates for the maneuvers, launch and arriving windows.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Multi-Objective Optimization of...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/3D537JA
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/3D537JA
Languageen
Target Filefaria_multi.pdf
User Grouplattes
marciana
Reader Groupadministrator
marciana
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
LinkingTrabalho Vinculado à Tese/Dissertação
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.45.41 1
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor format isbn issn lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject type url
7. Description control
e-Mail (login)marciana
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