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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3Q5932S
Repositorysid.inpe.br/mtc-m21b/2017/11.30.17.55   (restricted access)
Last Update2017:11.30.17.55.50 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2017/11.30.17.55.50
Metadata Last Update2021:02.11.18.12.59 (UTC) administrator
DOI10.1088/1742-6596/911/1/012022
ISSN1742-6588
Citation KeyGonçalvesRoccMora:2017:OrTrDe
TitleOrbital trajectories in deimos vicinity considering perturbations of gravitational origin
Year2017
Access Date2024, May 06
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size985 KiB
2. Context
Author1 Gonçalves, Liana Dias
2 Rocco, Evandro Marconi
3 Moraes, R. V. de
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
Group1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR
2 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Federal de São Paulo (UNIFESP)
Author e-Mail Address1 lianadgon@gmail.com
2 evandro.rocco@inpe.br
JournalJournal of Physics: Conference Series
Volume911
Pages012022
Secondary MarkB2_INTERDISCIPLINAR B2_ENGENHARIAS_III B3_MEDICINA_II B3_GEOCIÊNCIAS B4_MATERIAIS B4_ENGENHARIAS_II B4_BIOTECNOLOGIA C_QUÍMICA C_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA C_ENGENHARIAS_IV C_ECONOMIA C_ASTRONOMIA_/_FÍSICA
History (UTC)2017-11-30 17:55:50 :: simone -> administrator ::
2021-02-11 18:12:59 :: administrator -> simone :: 2017
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractThe present work studies the possibility of maintaining an artificial satellite near to the Deimos surface, even when considering the intense Mars gravitational attraction. For this, a strategy is used in which the spacecraft orbits Mars, but with the same orbital period of Deimos and similar orbital elements. Using this strategy, the deviations in the keplerian elements that characterize the artificial satellite orbit, the magnitude of the main disturbing forces capable of altering the movement of the spacecraft and the variation of the distance between the spacecraft and Deimos are presented.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Orbital trajectories in...
Arrangement 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbital trajectories in...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
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4. Conditions of access and use
Languageen
Target Filegoncalves_orbital.pdf
User Groupsimone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
DisseminationWEBSCI; PORTALCAPES; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn keywords label lineage mark mirrorrepository month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
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