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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3C63KNP
Repositorydpi.inpe.br/plutao/2012/06.21.18.26   (restricted access)
Last Update2012:08.24.13.52.23 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/06.21.18.26.15
Metadata Last Update2021:02.11.18.11.11 (UTC) administrator
DOI10.1155/2012/532708
ISSN1024-123X
1563-5147
Labellattes: 6880903376164690 1 GomesPrad:2012:LoOuOr
Citation KeyGomesPrad:2012:LoOuOr
TitleLow-Thrust Out-of-Plane Orbital Station-Keeping Maneuvers for Satellites
Year2012
Access Date2024, Mar. 28
Secondary TypePRE PI
Number of Files1
Size488 KiB
2. Context
Author1 Gomes, Vivian Martins
2 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
Group1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 vivian.gomes@uol.com.br
2 abertachini@terra.com.br
e-Mail Addressvivian.gomes@uol.com.br
JournalMathematical Problems in Engineering
Volume2012
NumberArticle ID 532708
Pages1-14
Secondary MarkB5_ASTRONOMIA_/_FÍSICA B4_CIÊNCIA_DA_COMPUTAÇÃO B3_CIÊNCIAS_AGRÁRIAS_I B1_ENGENHARIAS_I B2_ENGENHARIAS_II B1_ENGENHARIAS_III A2_ENGENHARIAS_IV A2_INTERDISCIPLINAR B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA
History (UTC)2012-06-22 00:10:59 :: lattes -> administrator :: 2012
2012-07-21 12:22:07 :: administrator -> secretaria.cpa@dir.inpe.br :: 2012
2012-12-14 11:15:52 :: secretaria.cpa@dir.inpe.br -> administrator :: 2012
2021-02-11 18:11:11 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsHybrid optimal control
Low thrust
Low-thrust propulsion
Numerical results
Orbital maneuvers
Out-of plane
Small amplitude
Station-keeping
AbstractThis paper considers the problem of out of plane orbital maneuvers for station keeping of satellites. The main idea is to consider that a satellite is in an orbit around the Earth and that it has its orbit is disturbed by one or more forces. Then, it is necessary to perform a small amplitude orbital correction to return the satellite to its original orbit, to keep it performing its mission. A low thrust propulsion is used to complete this task. It is important to search for solutions that minimize the fuel consumption to increase the lifetime of the satellite. To solve this problem a hybrid optimal control approach is used. The accuracy of the satisfaction of the constraints is considered, in order to try to decrease the fuel expenditure by taking advantage of this freedom. This type of problem presents numerical difficulties and it is necessary to adjust parameters, as well as details of the algorithm, to get convergence. In this versions of the algorithm that works well for planar maneuvers are usually not adequate for the out of plane orbital corrections. In order to illustrate the method, some numerical results are presented.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Low-Thrust Out-of-Plane Orbital...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target FileGomes&Prado_2012.pdf
User Groupadministrator
lattes
secretaria.cpa@dir.inpe.br
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
DisseminationPORTALCAPES
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel format isbn lineage mark mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marciana
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