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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/39RQD42
Repositorydpi.inpe.br/plutao/2011/06.11.03.18   (restricted access)
Last Update2011:10.18.10.55.33 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2011/06.11.03.18.01
Metadata Last Update2021:02.11.18.11.09 (UTC) administrator
Secondary KeyINPE--PRE/
DOI10.1155/2011/187478
ISSN1024-123X
1563-5147
Labellattes: 7340081273816424 3 CarvalhoMoraPrad:2011:ApMo
Citation KeyCarvalhoMoraPrad:2011:ApMo
TitlePlanetary Satellite Orbiters: Applications for the Moon
ProjectFAPESP, SP-Brazil[2007/04413-7, 2006/04997-6]; CNPQ[300952/2008-2]
Year2011
Access Date2024, May 05
Secondary TypePRE PI
Number of Files1
Size1957 KiB
2. Context
Author1 Carvalho, Jean P S
2 Moraes, Rodolpho Vilhena de
3 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGJA
Group1
2
3 DMC-ETE-INPE-MCT-BR
Affiliation1 Universidade Estadual Paulista (UNESP), 12 
2 Univ Fed Sao Paulo UNIFESP, Inst Ciencia & Tecnol, BR-12331280 Sao Jose Dos Campos, SP, Brazil
3 Instituto de Ciência e Tecnologia, Universidade Federal de São Paulo (UNIFESP), 12 
Author e-Mail Address1
2
3 abertachini@terra.com.br
e-Mail Addressabertachini@terra.com.br
JournalMathematical Problems in Engineering
Volume2011
NumberID 187478
Pages1-19
Secondary MarkB5_ASTRONOMIA_/_FÍSICA B4_CIÊNCIA_DA_COMPUTAÇÃO B3_CIÊNCIAS_AGRÁRIAS_I B1_ENGENHARIAS_I B2_ENGENHARIAS_II B1_ENGENHARIAS_III A2_ENGENHARIAS_IV A2_INTERDISCIPLINAR B3_MATEMÁTICA_/_PROBABILIDADE_E_ESTATÍSTICA
History (UTC)2011-06-11 17:43:44 :: lattes -> administrator :: 2011
2011-06-16 12:29:35 :: administrator -> marciana :: 2011
2012-01-17 15:06:37 :: marciana -> administrator :: 2011
2021-02-11 18:11:09 :: administrator -> marciana :: 2011
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodinâmica
Manobras Orbitais
Trajetórias Espaciais. LUNAR ARTIFICIAL-SATELLITE
GRAVITATIONAL-FIELD
PROSPECTOR MISSION
ANALYTICAL-MODEL
SCIENCE ORBITS
FROZEN ORBITS
EUROPA
AbstractLow-altitude, near-polar orbits are very desirable as science orbits for missions to planetary satellites, such as the Earth's Moon. In this paper, we present an analytical theory with numerical simulations to study the orbital motion of lunar low-altitude artificial satellite. We consider the problem of an artificial satellite perturbed by the nonuniform distribution of the mass of the Moon (J(2)-J(5), J(7), and C(22)). The conditions to get frozen orbits are presented. Using an approach that considers the single-averaged problem, we found families of periodic orbits for the problem of an orbiter travelling around the Moon, where frozen orbits valid for long periods of time are found. A comparison between the models for the zonal and tesseral harmonics coefficients is presented.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Planetary Satellite Orbiters:...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target File187478.pdf
User Groupadministrator
lattes
marciana
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
URL (untrusted data)http://www.hindawi.com/journals/mpe/2011/187478/
DisseminationPORTALCAPES
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 mirrorrepository month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress readergroup rightsholder schedulinginformation secondarydate session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Description control
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