Close

1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3KN33QE
Repositorysid.inpe.br/plutao/2015/12.04.13.49.06   (restricted access)
Last Update2015:12.11.11.35.35 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2015/12.04.13.49.07
Metadata Last Update2021:07.28.22.22.43 (UTC) administrator
DOI10.1088/1742-6596/641/1/012028
ISSN1742-6588
Labellattes: 0088337156908774 2 GonçalvesRoccMora:2015:AnInOr
Citation KeyGonçalvesRoccMora:2015:AnInOr
TitleAnalysis of the influence of orbital disturbances applied to an artificial lunar satellite
Year2015
Access Date2024, May 15
Type of Workconference paper
Secondary TypePRE PI
Number of Files1
Size1285 KiB
2. Context
Author1 Gonçalves, Liana Dias
2 Rocco, Evandro Marconi
3 Moraes, Rodolpho Vilhena de
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
Group1
2 DMC-ETE-INPE-MCTI-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
Volume641
Pages012028
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)2015-12-04 13:49:07 :: lattes -> administrator ::
2021-07-28 22:22:43 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodynamics
Orbit Perturbation
Orbital Motion
AbstractThis paper analyzes the influence of the orbital disturbance forces in the trajectory of lunar satellites. The following gravitational and non-gravitational orbital disturbances are considered: the non-homogeneity of the lunar gravitational field; the gravitational attraction due to the third body, considering the Earth and the Sun; the lunar albedo; the solar radiation pressure. Numerical models were developed and implemented in an orbital trajectory simulator aiming to understand the dynamics of the orbital motion of an artificial satellite in lunar orbit when considering the simultaneous effect of all disturbances. Different orbits were simulated in order to characterize the major and the minor influence of each disturbing force as function of the inclination and the right ascension of the ascending node. This study can be very useful in the space mission analysis and in the selection of orbits less affected by environmental disturbances.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Analysis of the...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languagept
Target File1_goncalves3.pdf
User Grouplattes
simone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft12
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.41 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 e-mailaddress format isbn lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Description control
e-Mail (login)simone
update 


Close