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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3E7UFNA
Repositorydpi.inpe.br/plutao/2013/05.31.17.32.41   (restricted access)
Last Update2013:07.17.13.59.24 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2013/05.31.17.32.42
Metadata Last Update2021:02.11.18.11.16 (UTC) administrator
DOI10.1155/2013/945030
ISSN1024-123X
Labellattes: 7340081273816424 4 OliveiraRoccFerrPrad:2013:MiFuLo
Citation KeyOliveiraRoccFerrPrad:2013:MiFuLo
TitleMinimum Fuel Low-Thrust Transfers for Satellites Using a Permanent Magnet Hall Thruster
Year2013
Access Date2024, May 16
Secondary TypePRE PI
Number of Files1
Size3544 KiB
2. Context
Author1 Oliveira, Thais Carneiro
2 Rocco, Evandro Marconi
3 Ferreira, José Leonardo
4 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
3
4 8JMKD3MGP5W/3C9JGJA
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
3
4 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade de Brasília, Campus Darcy Ribeiro, Plano Piloto, 70910-900 Asa Norte, DF, Brazil
4 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 evandro@dem.inpe.br
3
4 prado@dem.inpe.br
e-Mail Addressprado@dem.inpe.br
JournalMathematical Problems in Engineering
Volume2013
NumberID 945030
Pages1-12
Secondary MarkB1 B1 B1 B1 B1 B2 B3 B3 B4 B4 B5
History (UTC)2013-05-31 17:32:42 :: lattes -> administrator ::
2021-02-11 18:11:16 :: administrator -> marcelo.pazos@inpe.br :: 2013
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
Keywordssatellite missions
orbital maneuvers
permanent magnet hall thruster
AbstractMost of the satellite missions require orbital maneuvers to accomplish its goals. An orbital maneuver is an operation where the orbit of a satellite is changed, usually applying a type of propulsion. The maneuvers may have several purposes, such as the transfer of a satellite to its final orbit, the interception of another spacecraft, or the adjustment of the orbit to compensate the shifts caused by external forces. In this situation it is essential to minimize the fuel consumption to allow a greater number of maneuvers to be performed, and thus the lifetime of the satellite can be extended. There are several papers and studies which aim at the fuel minimization in maneuvers performed by space vehicles. In this context, this paper has two goals: (i) to develop an algorithm capable of finding optimal trajectories with continuous thrust that can fit different types of missions and constraints at the same time and (ii) to study the performance of two propulsion devices for orbital maneuvers under development at the Universidade de Brasilia, including a study of the effects of the errors in magnitude of these new devices.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Minimum Fuel Low-Thrust...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target File945030.pdf
User Groupadministrator
lattes
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 2
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 1
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
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 month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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