Optimization of satellite constellations in the moon
Autor(a) principal: | |
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Data de Publicação: | 2010 |
Outros Autores: | , , |
Tipo de documento: | Artigo de conferência |
Idioma: | eng |
Título da fonte: | Repositório Institucional da UNESP |
Texto Completo: | http://www.iafastro.net/iac/archive/browse/IAC-10/A3/2B/8458/ http://hdl.handle.net/11449/72168 |
Resumo: | Nowadays, we return to live a period of lunar exploration. China, Japan and India heavily invest in missions to the moon, and then try to implement manned bases on this satellite. These bases must be installed in polar regions due to the apparent existence of water. Therefore, the study of the feasibility of satellite constellations for navigation, control and communication recovers importance. The Moon's gravitational potential and resonant movements due to the proximity to Earth as the Kozai-Lidov resonance, must be considered in addition to other perturbations of lesser magnitude. The usual satellite constellations provide, as a basic feature, continuous and global coverage of the Earth. With this goal, they are designed for the smallest number of objects possible to perform a specific task and this amount is directly related to the altitude of the orbits and visual abilities of the members of the constellation. However the problem is different when the area to be covered is reduced to a given zone. The required number of space objects can be reduced. Furthermore, depending on the mission requirements it may be not necessary to provide continuous coverage. Taking into account the possibility of setting up a constellation that covers a specific region of the Moon on a non-continuous base, in this study we seek a criterion of optimization related to the time between visits. The propagation of the orbits of objects in the constellation in conjunction with the coverage constraints, provide information on the periods of time in which points of the surface are covered by a satellite, and time intervals in which they are not. So we minimize the time between visits considering several sets of possible constellations and using genetic algorithms. |
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Optimization of satellite constellations in the moonConstellationGenetic algorithmLunar potentialContinuous coverageGlobal coverageGravitational potentialMission requirementsPolar RegionsSatellite constellationsSpace objectsSpecific tasksTime intervalVisual abilitiesGenetic algorithmsLunar missionsOptimizationSatellitesNowadays, we return to live a period of lunar exploration. China, Japan and India heavily invest in missions to the moon, and then try to implement manned bases on this satellite. These bases must be installed in polar regions due to the apparent existence of water. Therefore, the study of the feasibility of satellite constellations for navigation, control and communication recovers importance. The Moon's gravitational potential and resonant movements due to the proximity to Earth as the Kozai-Lidov resonance, must be considered in addition to other perturbations of lesser magnitude. The usual satellite constellations provide, as a basic feature, continuous and global coverage of the Earth. With this goal, they are designed for the smallest number of objects possible to perform a specific task and this amount is directly related to the altitude of the orbits and visual abilities of the members of the constellation. However the problem is different when the area to be covered is reduced to a given zone. The required number of space objects can be reduced. Furthermore, depending on the mission requirements it may be not necessary to provide continuous coverage. Taking into account the possibility of setting up a constellation that covers a specific region of the Moon on a non-continuous base, in this study we seek a criterion of optimization related to the time between visits. The propagation of the orbits of objects in the constellation in conjunction with the coverage constraints, provide information on the periods of time in which points of the surface are covered by a satellite, and time intervals in which they are not. So we minimize the time between visits considering several sets of possible constellations and using genetic algorithms.São Paulo State University (UNESP), Guaratinguetá - SPUniversidad Nacional de Córdoba, CórdobaIsrael Institute of Tecnology, HaifaSão Paulo State University (UNESP), Guaratinguetá - SPUniversidade Estadual Paulista (Unesp)Universidad Nacional de CórdobaIsrael Institute of TecnologyWinter, Othon C. [UNESP]Schulz, W.Izidoro, A. [UNESP]Mazal, L.2014-05-27T11:25:24Z2014-05-27T11:25:24Z2010-12-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject2991-2995http://www.iafastro.net/iac/archive/browse/IAC-10/A3/2B/8458/61st International Astronautical Congress 2010, IAC 2010, v. 4, p. 2991-2995.http://hdl.handle.net/11449/721682-s2.0-79959446903Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPeng61st International Astronautical Congress 2010, IAC 2010info:eu-repo/semantics/openAccess2024-07-02T14:29:48Zoai:repositorio.unesp.br:11449/72168Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462024-08-05T18:50:14.087687Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
Optimization of satellite constellations in the moon |
title |
Optimization of satellite constellations in the moon |
spellingShingle |
Optimization of satellite constellations in the moon Winter, Othon C. [UNESP] Constellation Genetic algorithm Lunar potential Continuous coverage Global coverage Gravitational potential Mission requirements Polar Regions Satellite constellations Space objects Specific tasks Time interval Visual abilities Genetic algorithms Lunar missions Optimization Satellites |
title_short |
Optimization of satellite constellations in the moon |
title_full |
Optimization of satellite constellations in the moon |
title_fullStr |
Optimization of satellite constellations in the moon |
title_full_unstemmed |
Optimization of satellite constellations in the moon |
title_sort |
Optimization of satellite constellations in the moon |
author |
Winter, Othon C. [UNESP] |
author_facet |
Winter, Othon C. [UNESP] Schulz, W. Izidoro, A. [UNESP] Mazal, L. |
author_role |
author |
author2 |
Schulz, W. Izidoro, A. [UNESP] Mazal, L. |
author2_role |
author author author |
dc.contributor.none.fl_str_mv |
Universidade Estadual Paulista (Unesp) Universidad Nacional de Córdoba Israel Institute of Tecnology |
dc.contributor.author.fl_str_mv |
Winter, Othon C. [UNESP] Schulz, W. Izidoro, A. [UNESP] Mazal, L. |
dc.subject.por.fl_str_mv |
Constellation Genetic algorithm Lunar potential Continuous coverage Global coverage Gravitational potential Mission requirements Polar Regions Satellite constellations Space objects Specific tasks Time interval Visual abilities Genetic algorithms Lunar missions Optimization Satellites |
topic |
Constellation Genetic algorithm Lunar potential Continuous coverage Global coverage Gravitational potential Mission requirements Polar Regions Satellite constellations Space objects Specific tasks Time interval Visual abilities Genetic algorithms Lunar missions Optimization Satellites |
description |
Nowadays, we return to live a period of lunar exploration. China, Japan and India heavily invest in missions to the moon, and then try to implement manned bases on this satellite. These bases must be installed in polar regions due to the apparent existence of water. Therefore, the study of the feasibility of satellite constellations for navigation, control and communication recovers importance. The Moon's gravitational potential and resonant movements due to the proximity to Earth as the Kozai-Lidov resonance, must be considered in addition to other perturbations of lesser magnitude. The usual satellite constellations provide, as a basic feature, continuous and global coverage of the Earth. With this goal, they are designed for the smallest number of objects possible to perform a specific task and this amount is directly related to the altitude of the orbits and visual abilities of the members of the constellation. However the problem is different when the area to be covered is reduced to a given zone. The required number of space objects can be reduced. Furthermore, depending on the mission requirements it may be not necessary to provide continuous coverage. Taking into account the possibility of setting up a constellation that covers a specific region of the Moon on a non-continuous base, in this study we seek a criterion of optimization related to the time between visits. The propagation of the orbits of objects in the constellation in conjunction with the coverage constraints, provide information on the periods of time in which points of the surface are covered by a satellite, and time intervals in which they are not. So we minimize the time between visits considering several sets of possible constellations and using genetic algorithms. |
publishDate |
2010 |
dc.date.none.fl_str_mv |
2010-12-01 2014-05-27T11:25:24Z 2014-05-27T11:25:24Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/conferenceObject |
format |
conferenceObject |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://www.iafastro.net/iac/archive/browse/IAC-10/A3/2B/8458/ 61st International Astronautical Congress 2010, IAC 2010, v. 4, p. 2991-2995. http://hdl.handle.net/11449/72168 2-s2.0-79959446903 |
url |
http://www.iafastro.net/iac/archive/browse/IAC-10/A3/2B/8458/ http://hdl.handle.net/11449/72168 |
identifier_str_mv |
61st International Astronautical Congress 2010, IAC 2010, v. 4, p. 2991-2995. 2-s2.0-79959446903 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
61st International Astronautical Congress 2010, IAC 2010 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/openAccess |
eu_rights_str_mv |
openAccess |
dc.format.none.fl_str_mv |
2991-2995 |
dc.source.none.fl_str_mv |
Scopus reponame:Repositório Institucional da UNESP instname:Universidade Estadual Paulista (UNESP) instacron:UNESP |
instname_str |
Universidade Estadual Paulista (UNESP) |
instacron_str |
UNESP |
institution |
UNESP |
reponame_str |
Repositório Institucional da UNESP |
collection |
Repositório Institucional da UNESP |
repository.name.fl_str_mv |
Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP) |
repository.mail.fl_str_mv |
|
_version_ |
1808128988445409280 |