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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3Q592C5
Repositorysid.inpe.br/mtc-m21b/2017/11.30.17.47   (restricted access)
Last Update2017:11.30.17.47.33 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2017/11.30.17.47.33
Metadata Last Update2021:02.11.18.12.57 (UTC) administrator
DOI10.1088/1742-6596/911/1/012014
ISSN1742-6588
Citation KeyMeirelesRocc:2017:StOrTr
TitleStudy of orbital transfers with time constraint and fuel optimization
Year2017
Access Date2024, May 16
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size6498 KiB
2. Context
Author1 Meireles, L. G.
2 Rocco, Evandro Marconi
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
Group1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR
2 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 meireleslg@gmail.com
2 evandro.rocco@inpe.br
JournalJournal of Physics: Conference Series
Volume911
Pages012014
Secondary MarkB2_INTERDISCIPLINAR B2_ENGENHARIAS_III B3_MEDICINA_II B3_GEOCIÊNCIAS B4_MATERIAIS B4_ENGENHARIAS_II B4_BIOTECNOLOGIA C_QUÍMICA C_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA C_ENGENHARIAS_IV C_ECONOMIA C_ASTRONOMIA_/_FÍSICA
History (UTC)2017-11-30 17:47:33 :: simone -> administrator ::
2021-02-11 18:12:57 :: administrator -> simone :: 2017
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractOver the decades, with the advance in computational power and the development of new optimization techniques, a new opportunity arose for a reviewed approach and analysis of already existing solutions to orbital transfer problems. With that in mind, a study was proposed over Lambert's problem of bi-impulsive orbital transfers with time constraint for the execution of minimum fuel maneuvers between coplanar and non coplanar elliptical orbits. In order to achieve this goal, a genetic search algorithm was developed to determine the minimum fuel trajectory with an iterative variation of two Keplerian elements of the final orbit, one of them being the mean anomaly and the other a choice between the eccentricity, the inclination or the argument of periapsis. A number of six simulations were performed under these conditions, using different values - on each simulation - for the Keplerian elements of the final orbits not being iteratively varied. Remarkable sections were noted regarding the behaviour of fuel consumption values of the minimum fuel trajectories. One of which was a noted relation between the lowest cost minimum fuel transfers and the ratio of the semi-major axis and eccentricity of these transfers' initial and final orbits, considering both the orbits have the same value of argument of periapsis. Amongst all simulations, it was important to identify the choice between short or long way for the determination of the minimum fuel transfer, analysing the implications of that choice on the transfer time.
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Arrangement 1urlib.net > CMC > Study of orbital...
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4. Conditions of access and use
Languageen
Target Filemeireles_study.pdf
User Groupsimone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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