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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP5W34M/3HE6FJM
Repositorysid.inpe.br/mtc-m21b/2014/11.19.00.00.46   (restricted access)
Last Update2015:02.09.18.32.13 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2014/11.19.00.00.47
Metadata Last Update2018:06.04.03.04.34 (UTC) administrator
DOI10.1016/j.asr.2014.07.018
ISSN0273-1177
1879-1948
Labelscopus 2014-11 SalazarMasGómMacWin:2014:ZeMiMa
Citation KeySalazarMasGómMacWin:2014:ZeMiMa
TitleZero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon system
Year2014
Access Date2024, June 15
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size6248 KiB
2. Context
Author1 Salazar, F. J. T.
2 Masdemont, J. J.
3 Gómez, G.
4 Macau, Elbert Einstein Nehrer
5 Winter, O. C.
Resume Identifier1
2
3
4 8JMKD3MGP5W/3C9JGUT
Group1
2
3
4 LAC-CTE-INPE-MCTI-GOV-BR
Affiliation1 Universidade Estadual Paulista (UNESP)
2 ETSEIB-UPC
3 Departament de Matemàtica Aplicada i Anàlisi, UB
4 Instituto Nacional de Pesquisas Espaciais (INPE)
5 Universidade Estadual Paulista (UNESP)
Author e-Mail Address1 e7940@hotmail.com
2 josep@barquins.upc.edu
3 gerard@maia.ub.es
4 elbert.macau@inpe.br
5 ocwinter@gmail.com
e-Mail Addressmarcelo.pazos@inpe.br
JournalAdvances in Space Research
Volume54
Number9
Pages1838-1857
History (UTC)2018-06-04 03:04:34 :: administrator -> marcelo.pazos@inpe.br :: 2014
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractAssume a constellation of satellites is flying near a given nominal trajectory around L4 or L5 in the Earth-Moon system in such a way that there is some freedom in the selection of the geometry of the constellation. We are interested in avoiding large variations of the mutual distances between spacecraft. In this case, the existence of regions of zero and minimum relative radial acceleration with respect to the nominal trajectory will prevent from the expansion or contraction of the constellation. In the other case, the existence of regions of maximum relative radial acceleration with respect to the nominal trajectory will produce a larger expansion and contraction of the constellation. The goal of this paper is to study these regions in the scenario of the Circular Restricted Three Body Problem by means of a linearization of the equations of motion relative to the periodic orbits around L4 or L5. This study corresponds to a preliminar planar formation flight dynamics about triangular libration points in the Earth-Moon system. Additionally, the cost estimate to maintain the constellation in the regions of zero and minimum relative radial acceleration or keeping a rigid configuration is computed with the use of the residual acceleration concept. At the end, the results are compared with the dynamical behavior of the deviation of the constellation from a periodic orbit.
AreaCOMP
ArrangementZero, minimum and...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
User Groupadministrator
marcelo.pazos@inpe.br
Reader Groupadministrator
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Visibilityshown
Archiving Policydenypublisher denyfinaldraft24
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
LinkingTrabalho não Vinculado à Tese/Dissertação
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/3ESGTTP
Citing Item Listsid.inpe.br/bibdigital/2013/09.22.23.14 4
sid.inpe.br/mtc-m21/2012/07.13.14.45.07 2
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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