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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3JJPAUK
Repositorysid.inpe.br/plutao/2015/06.01.12.19.11   (restricted access)
Last Update2015:07.06.15.02.22 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2015/06.01.12.19.12
Metadata Last Update2018:06.04.23.25.36 (UTC) administrator
DOI10.1016/j.asr.2015.03.028
ISSN0273-1177
1879-1948
Labellattes: 0793627832164040 3 SalazarWinMacMasGóm:2015:NaFoEa
Citation KeySalazarWinMacMasGóm:2015:NaFoEa
TitleNatural formations at the Earth-Moon triangular point in perturbed restricted problems
Year2015
Access Date2024, May 28
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size5318 KiB
2. Context
Author1 Salazar, F. J. T.
2 Winter, O. C.
3 Macau, Elbert Einstein Nehrer
4 Masdemont, J. J.
5 Gómez, G.
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JGUT
Group1
2
3 LAC-CTE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2 Universidade Estadual Paulista (UNESP)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
4 ETSEIB-UPC
5 Departament de Matemàtica Aplicada i Anàisi, UB
Author e-Mail Address1
2
3 elbert.macau@inpe.br
JournalAdvances in Space Research
Volume56
Pages144-162
Secondary MarkB1_ENGENHARIAS_IV B1_ENGENHARIAS_III B1_GEOCIÊNCIAS B1_BIODIVERSIDADE B1_INTERDISCIPLINAR B3_CIÊNCIA_DA_COMPUTAÇÃO B4_ASTRONOMIA_/_FÍSICA C_CIÊNCIAS_BIOLÓGICAS_I
History (UTC)2015-06-01 12:19:12 :: lattes -> administrator ::
2018-06-04 23:25:36 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsDinamica Nao-Linear
Dinâmica Orbital
Astrodinâmica
controle
Dinâmica Caótica
AbstractPrevious studies for small formation flying dynamics about triangular libration points have determined the existence of regions of zero and Minimum Relative Radial Acceleration with respect to the nominal trajectory, that prevent from the expansion or contraction of the constellation. However, these studies only considered the gravitational force of the Earth and the Moon using the Circular Restricted Three Body Problem (CRTBP) scenario. Although the CRTBP model is a good approximation for the dynamics of spacecraft in the EarthMoon system, the nominal trajectories around equilateral libration points are strongly affected when the primary orbit eccentricity and solar gravitational force are considered. In this manner, the goal of this work is the analysis of the best regions to place a formation that is flying close a bounded solution around L4, taking into account the Moons eccentricity and Suns gravity. This model is not only more realistic for practical engineering applications but permits to determine more accurately the fuel consumption to maintain the geometry of the formation.
AreaCOMP
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Natural formations at...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filesalazar_natural.pdf
User Grouplattes
simone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft24
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/3ESGTTP
Citing Item Listsid.inpe.br/bibdigital/2013/09.22.23.14 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.07 2
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn lineage mark month nextedition number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
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