Natural formations at the Earth-Moon triangular point in perturbed restricted problems

Previous 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...

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Detalles Bibliográficos
Autores: Salazar, Francisco, Winter, O. C., Macau, E.E.N., Masdemont Soler, Josep|||0000-0002-3456-1127, Gómez Muntané, Gerard
Tipo de recurso: artículo
Fecha de publicación:2015
País:España
Institución:Universitat Politècnica de Catalunya (UPC)
Repositorio:UPCommons. Portal del coneixement obert de la UPC
Idioma:inglés
OAI Identifier:oai:upcommons.upc.edu:2117/84940
Acceso en línea:https://hdl.handle.net/2117/84940
https://dx.doi.org/10.1016/j.asr.2015.03.028
Access Level:acceso abierto
Palabra clave:Orbital mechanics
Artificial satellites--Control systems
Earth (Planet)
Moon
Formation flight of satellites
Zero Relative Radial Acceleration
Earth-Moon system
Elliptic Restricted Three Body Problem
Bicircular Four Body Problem
Equilateral libration point
libration point
formation flight
motion
dynamics
stability
evolution
mission
orbits
bodies
system
Satèl·lits artificials
Terra (Planeta)
Lluna
Àrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciències
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repository_id_str
spelling Natural formations at the Earth-Moon triangular point in perturbed restricted problemsSalazar, FranciscoWinter, O. C.Macau, E.E.N.Masdemont Soler, Josep|||0000-0002-3456-1127Gómez Muntané, GerardOrbital mechanicsArtificial satellites--Control systemsEarth (Planet)MoonFormation flight of satellitesZero Relative Radial AccelerationEarth-Moon systemElliptic Restricted Three Body ProblemBicircular Four Body ProblemEquilateral libration pointlibration pointformation flightmotiondynamicsstabilityevolutionmissionorbitsbodiessystemSatèl·lits artificialsTerra (Planeta)LlunaÀrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciènciesPrevious 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 Earth-Moon 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 L-4, taking into account the Moon's eccentricity and Sun's 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. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.20152015-07-0120162016-03-31journal articlehttp://purl.org/coar/resource_type/c_6501AMhttp://purl.org/coar/version/c_ab4af688f83e57aainfo:eu-repo/semantics/articleapplication/pdfhttps://hdl.handle.net/2117/84940https://dx.doi.org/10.1016/j.asr.2015.03.028reponame:UPCommons. Portal del coneixement obert de la UPCinstname:Universitat Politècnica de Catalunya (UPC)InglésengMinisterio de Economía y Competitividad http://doi.org/10.13039/501100003329 MTM2012-31714 DINAMICA ASOCIADA A CONEXIONES ENTRE OBJETOS INVARIANTES. APLICACIONES A ASTRODINAMICA, NEUROCIENCIA Y OTROS CAMPOSopen accesshttp://purl.org/coar/access_right/c_abf2http://creativecommons.org/licenses/by-nc-nd/3.0/es/info:eu-repo/semantics/openAccessoai:upcommons.upc.edu:2117/849402026-05-27T15:37:01Z
dc.title.none.fl_str_mv Natural formations at the Earth-Moon triangular point in perturbed restricted problems
title Natural formations at the Earth-Moon triangular point in perturbed restricted problems
spellingShingle Natural formations at the Earth-Moon triangular point in perturbed restricted problems
Salazar, Francisco
Orbital mechanics
Artificial satellites--Control systems
Earth (Planet)
Moon
Formation flight of satellites
Zero Relative Radial Acceleration
Earth-Moon system
Elliptic Restricted Three Body Problem
Bicircular Four Body Problem
Equilateral libration point
libration point
formation flight
motion
dynamics
stability
evolution
mission
orbits
bodies
system
Satèl·lits artificials
Terra (Planeta)
Lluna
Àrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciències
title_short Natural formations at the Earth-Moon triangular point in perturbed restricted problems
title_full Natural formations at the Earth-Moon triangular point in perturbed restricted problems
title_fullStr Natural formations at the Earth-Moon triangular point in perturbed restricted problems
title_full_unstemmed Natural formations at the Earth-Moon triangular point in perturbed restricted problems
title_sort Natural formations at the Earth-Moon triangular point in perturbed restricted problems
dc.creator.none.fl_str_mv Salazar, Francisco
Winter, O. C.
Macau, E.E.N.
Masdemont Soler, Josep|||0000-0002-3456-1127
Gómez Muntané, Gerard
author Salazar, Francisco
author_facet Salazar, Francisco
Winter, O. C.
Macau, E.E.N.
Masdemont Soler, Josep|||0000-0002-3456-1127
Gómez Muntané, Gerard
author_role author
author2 Winter, O. C.
Macau, E.E.N.
Masdemont Soler, Josep|||0000-0002-3456-1127
Gómez Muntané, Gerard
author2_role author
author
author
author
dc.subject.none.fl_str_mv Orbital mechanics
Artificial satellites--Control systems
Earth (Planet)
Moon
Formation flight of satellites
Zero Relative Radial Acceleration
Earth-Moon system
Elliptic Restricted Three Body Problem
Bicircular Four Body Problem
Equilateral libration point
libration point
formation flight
motion
dynamics
stability
evolution
mission
orbits
bodies
system
Satèl·lits artificials
Terra (Planeta)
Lluna
Àrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciències
topic Orbital mechanics
Artificial satellites--Control systems
Earth (Planet)
Moon
Formation flight of satellites
Zero Relative Radial Acceleration
Earth-Moon system
Elliptic Restricted Three Body Problem
Bicircular Four Body Problem
Equilateral libration point
libration point
formation flight
motion
dynamics
stability
evolution
mission
orbits
bodies
system
Satèl·lits artificials
Terra (Planeta)
Lluna
Àrees temàtiques de la UPC::Matemàtiques i estadística::Matemàtica aplicada a les ciències
description Previous 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 Earth-Moon 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 L-4, taking into account the Moon's eccentricity and Sun's 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. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.
publishDate 2015
dc.date.none.fl_str_mv 2015
2015-07-01
2016
2016-03-31
dc.type.none.fl_str_mv journal article
http://purl.org/coar/resource_type/c_6501
AM
http://purl.org/coar/version/c_ab4af688f83e57aa
dc.type.openaire.fl_str_mv info:eu-repo/semantics/article
format article
dc.identifier.none.fl_str_mv https://hdl.handle.net/2117/84940
https://dx.doi.org/10.1016/j.asr.2015.03.028
url https://hdl.handle.net/2117/84940
https://dx.doi.org/10.1016/j.asr.2015.03.028
dc.language.none.fl_str_mv Inglés
eng
language_invalid_str_mv Inglés
language eng
dc.relation.none.fl_str_mv Ministerio de Economía y Competitividad http://doi.org/10.13039/501100003329 MTM2012-31714 DINAMICA ASOCIADA A CONEXIONES ENTRE OBJETOS INVARIANTES. APLICACIONES A ASTRODINAMICA, NEUROCIENCIA Y OTROS CAMPOS
dc.rights.none.fl_str_mv open access
http://purl.org/coar/access_right/c_abf2

http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.rights.openaire.fl_str_mv info:eu-repo/semantics/openAccess
rights_invalid_str_mv open access
http://purl.org/coar/access_right/c_abf2

http://creativecommons.org/licenses/by-nc-nd/3.0/es/
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.source.none.fl_str_mv reponame:UPCommons. Portal del coneixement obert de la UPC
instname:Universitat Politècnica de Catalunya (UPC)
instname_str Universitat Politècnica de Catalunya (UPC)
reponame_str UPCommons. Portal del coneixement obert de la UPC
collection UPCommons. Portal del coneixement obert de la UPC
repository.name.fl_str_mv
repository.mail.fl_str_mv
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