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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3E7UFLP
Repositorydpi.inpe.br/plutao/2013/05.31.17.32
Last Update2013:06.24.18.39.09 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2013/05.31.17.32.31
Metadata Last Update2021:02.11.18.11.15 (UTC) administrator
ISSN1991-8747
Labellattes: 7340081273816424 2 RoccoPradSouz:2013:ThTwOr
Citation KeyRoccoPradSouz:2013:ThTwOr
TitleThree-dimensional two-impulsive orbital maneuvers with time limit
Year2013
MonthJan.
Access Date2024, Apr. 26
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size833 KiB
2. Context
Author1 Rocco, Evandro Marconi
2 Prado, Antonio Fernando Bertachini de Almeida
3 Souza, Marcelo Lopes Oliveira e
Resume Identifier1 8JMKD3MGP5W/3C9JH37
2 8JMKD3MGP5W/3C9JGJA
Group1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 evandro@dem.inpe.br
2 prado@dem.inpe.br
3 marcelo@dem.inpe.br
e-Mail Addressprado@dem.inpe.br
JournalWSEAS Transactions on Applied and Theoretical Mechanics
Volume8
Number1
Pages84-97
Secondary MarkB2
History (UTC)2013-05-31 17:32:31 :: lattes -> administrator ::
2021-02-11 18:11:15 :: 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
Keywordsorbital maneuvers
astrodynamics
impulsive control
AbstractThe problem of three-dimensional two-impulsive orbital maneuvers between two elliptical orbits with minimum fuel consumption, but having a time limit, is considered in the present paper. This limit in the time generates a new characteristic to the problem, which eliminates the majority of the methods available in the literature. Equations available in the literature are used and some new ones are developed to consider cases with different geometries. Those equations are then solved and a software is implemented to perform the orbital maneuvers. The original equations are presented in the literature without any numerical results, so, the new cases considered and the solutions and implementation of the method available in the literatures are the contributions shown here. The software was used with success in several different situations.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Three-dimensional two-impulsive orbital...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/3E7UFLP
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/3E7UFLP
Languageen
Target File56-490.pdf
User Grouplattes
marcelo.pazos@inpe.br
self-uploading-INPE-MCTI-GOV-BR
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
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/mtc-m21/2012/07.13.14.45.41 5
sid.inpe.br/bibdigital/2021/02.11.18.06 2
DisseminationCOMPENDEX; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi format isbn lineage mark nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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