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1. Identity statement
Reference TypeJournal Article
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Siteplutao.sid.inpe.br (namespace prefix: upn:33M4QT8)
IdentifierJ8LNKAN8RW/36G83MB
Repositorydpi.inpe.br/plutao@80/2009/11.30.19.54
Last Update2010:03.15.13.36.23 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao@80/2009/11.30.19.54.15
Metadata Last Update2021:02.11.18.11.18 (UTC) administrator
Secondary KeyINPE--PRE/
ISSN1991-8747
Labellattes: 7340081273816424 2 GomesPradKuga:2009:LoThMa
Citation KeyGomesPradKuga:2008:LoThMa
TitleLow thrust maneuvers for artificial satellites
Year2008
Access Date2026, Oct. 24
Secondary TypePRE PI
Number of Files1
Size310 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
2 DMC-ETE-INPE-MCT-BR
3 DMC-ETE-INPE-MCT-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 abertachini@terra.com.br
e-Mail Addressabertachini@terra.com.br
JournalWSEAS Transactions on Applied and Theoretical Mechanics
Volume3
Number10
Pages859-868
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01 upn:33M4QT8
History (UTC)2009-12-07 14:15:01 :: lattes -> marciana ::
2010-03-15 13:37:11 :: marciana -> administrator ::
2010-05-12 02:54:37 :: administrator -> marciana ::
2011-05-20 05:36:19 :: marciana -> administrator ::
2021-02-11 18:11:18 :: administrator -> marciana :: 2008
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsOrbital maneuvers
low thrust
astrodynamics
artificial satellites
orbital dynamics
AbstractAn orbital maneuver is an important phase of a space mission. The idea is to change the orbit of a spacecraft, in order to be able to complete the mission goals required. It can be done to insert a spacecraft in its nominal orbit or during the mission to compensate undesired effects of perturbations. To perform the orbital maneuvers, a software that calculates an optimal maneuver is developed. This method will be used as a reference for comparison and analises of the suboptimal methods to be used on board. This method id based on an analytical development that generate equations that can be computed in a shorter time, allowing real time applications. In all the simulations, low thrust is used to make the maneuvers.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Low thrust maneuvers...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URIupn:33M4QT8:J8LNKAN8RW/36G83MB
data URLhttp://urlib.net/ibi/J8LNKAN8RW/36G83MB
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/36G83MB
Target FileLow Thrust Maneuvers29-110.pdf
User Groupadministrator
lattes
marciana
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Read Permissionallow from all
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 - 64
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 - 19
sid.inpe.br/mtc-m21/2012/07.13.14.49.46 - 17
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination documentstage doi format isbn language lineage mark mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url versiontype
7. Description control
e-Mail (login)marciana
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