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1. Identity statement
Reference TypeJournal Article
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Sitemtc-m16b.sid.inpe.br (namespace prefix: upn:K28A8B)
Identifier6qtX3pFwXQZGivnK2Y/ShrvD
Repositorysid.inpe.br/mtc-m17@80/2007/11.27.13.41   (restricted access)
Last Update2007:11.27.13.41.35 (UTC) marciana
Metadata Repositorysid.inpe.br/mtc-m17@80/2007/11.27.13.41.36
Metadata Last Update2021:02.11.18.12.04 (UTC) administrator
Secondary KeyINPE--PRE/
DOI10.1155/2007/98532
ISSN1024-123X
1563-5147
Citation KeyGomesPradKuga:2007:OrMaUs
TitleOrbital Maneuvers Using Low Thrust to Place a Satellite in a Constellation
Year2007
Access Date2026, Apr. 19
Secondary TypePRE PI
Number of Files1
Size152 KiB
2. Context
Author1 Gomes, Vivian Martins
2 Prado, Antonio Fernando Bertachini de Almeida
3 Kuga, Helio Koiti
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
3 8JMKD3MGP5W/3C9JHC9
Group1 DMC-INPE-MCT-BR
2 DMC-INPE-MCT-BR
3 DMC-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
JournalMathematical Problems in Engineering
VolumeArticle ID 98532
Host Collectionlcp.inpe.br/ignes/2004/02.12.18.39 upn:LNRMAL
cptec.inpe.br/walmeida/2003/04.25.17.12 upn:K28A8B
History (UTC)2007-11-27 13:46:35 :: marciana -> administrator ::
2010-05-11 02:11:43 :: administrator -> marciana ::
2011-05-29 09:53:46 :: marciana -> administrator :: 2007
2014-08-15 02:38:03 :: administrator -> marciana :: 2007
2014-08-19 16:50:46 :: marciana -> administrator :: 2007
2021-02-11 18:12:04 :: administrator -> marciana :: 2007
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractThis paper considers the problem of low thrust suboptimal maneuvers to insert a satellite in a constellation. It is assumed that a satellite constellation is given with all the Keplerian elements of the satellite members having known values. Then, it is necessary to maneuver a new satellite from a parking orbit to its position in the constellation. The control available to perform this maneuver is the application of a low thrust to the satellite and the objective is to perform this maneuver with minimum fuel consumption.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital Maneuvers Using...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target FileS1024123X07985324[1].pdf
User Groupadministrator
marciana
Reader Groupadministrator
marciana
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 - 19
sid.inpe.br/mtc-m21/2012/07.13.14.49.46 - 8
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 6
DisseminationWEBSCI; PORTALCAPES; COMPENDEX.
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress electronicmailaddress format isbn keywords label lineage mark mirrorrepository month nextedition notes number orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marciana
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