STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS

Detalhes bibliográficos
Autor(a) principal: Prado, A. F. B. A.
Data de Publicação: 2016
Outros Autores: Cardoso dos Santos, J. [UNESP], Carvalho, J. P. S., Vilhena de Moraes, R., Zanetti, R., Russell, R. P., Ozimek, M. T., Bowes, A. L.
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://hdl.handle.net/11449/159575
Resumo: Several scientific missions have been proposed for a deeper exploration of planetary systems. These missions require a lot of specialized techniques in order to reach a better understanding of the dynamics involved in their planning. In order to help to get important features about each system under study, the present study proposes to use different definitions of integrals of the perturbing forces received by spacecrafts to help to find the best orbits for them. These computations present important information about the level of perturbation acting in the spacecraft due to the effects of each force considered in the system and they also help to understand the evolution of these perturbations. The system of Galilean moons is explored to test these techniques.
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spelling STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONSSeveral scientific missions have been proposed for a deeper exploration of planetary systems. These missions require a lot of specialized techniques in order to reach a better understanding of the dynamics involved in their planning. In order to help to get important features about each system under study, the present study proposes to use different definitions of integrals of the perturbing forces received by spacecrafts to help to find the best orbits for them. These computations present important information about the level of perturbation acting in the spacecraft due to the effects of each force considered in the system and they also help to understand the evolution of these perturbations. The system of Galilean moons is explored to test these techniques.UNESPUFRBINPEUNIFESPConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Natl Inst Space Res INPE, INPE Brazil, Board Grad Sch, Sao Jose Dos Campos, BrazilSao Paulo State Univ, UNESP, Guaratingueta, BrazilUniv Colorado, CCAR UCB, Boulder, CO 80309 USAFed Univ Reconcavo Bahia UFRB, Ctr Energy & Sustainabil Sci & Technol, Feira De Santana, BrazilFed Univ Sao Paulo UNIFESP, Inst Sci & Technol, Sao Jose Dos Campos, BrazilSao Paulo State Univ, UNESP, Guaratingueta, BrazilCNPq: 306953/2014-5FAPESP: 2015/18881-9FAPESP: 2014/06688-7FAPESP: 2013/26652-4FAPESP: 2012/21023-6FAPESP: 2011/05671-5FAPESP: 2011/08171-3Univelt IncNatl Inst Space Res INPEUniversidade Estadual Paulista (Unesp)Univ ColoradoFed Univ Reconcavo Bahia UFRBUniversidade de São Paulo (USP)Prado, A. F. B. A.Cardoso dos Santos, J. [UNESP]Carvalho, J. P. S.Vilhena de Moraes, R.Zanetti, R.Russell, R. P.Ozimek, M. T.Bowes, A. L.2018-11-26T15:44:20Z2018-11-26T15:44:20Z2016-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject1565-1583Spaceflight Mechanics 2016, Pts I-iv. San Diego: Univelt Inc, v. 158, p. 1565-1583, 2016.1081-6003http://hdl.handle.net/11449/159575WOS:000403301400090Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengSpaceflight Mechanics 2016, Pts I-ivinfo:eu-repo/semantics/openAccess2021-10-23T21:44:25Zoai:repositorio.unesp.br:11449/159575Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-23T21:44:25Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
title STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
spellingShingle STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
Prado, A. F. B. A.
title_short STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
title_full STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
title_fullStr STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
title_full_unstemmed STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
title_sort STUDY OF PERTURBATION INTEGRALS APPLIED TO THE DYNAMICS OF SPACECRAFTS AROUND GALILEAN MOONS
author Prado, A. F. B. A.
author_facet Prado, A. F. B. A.
Cardoso dos Santos, J. [UNESP]
Carvalho, J. P. S.
Vilhena de Moraes, R.
Zanetti, R.
Russell, R. P.
Ozimek, M. T.
Bowes, A. L.
author_role author
author2 Cardoso dos Santos, J. [UNESP]
Carvalho, J. P. S.
Vilhena de Moraes, R.
Zanetti, R.
Russell, R. P.
Ozimek, M. T.
Bowes, A. L.
author2_role author
author
author
author
author
author
author
dc.contributor.none.fl_str_mv Natl Inst Space Res INPE
Universidade Estadual Paulista (Unesp)
Univ Colorado
Fed Univ Reconcavo Bahia UFRB
Universidade de São Paulo (USP)
dc.contributor.author.fl_str_mv Prado, A. F. B. A.
Cardoso dos Santos, J. [UNESP]
Carvalho, J. P. S.
Vilhena de Moraes, R.
Zanetti, R.
Russell, R. P.
Ozimek, M. T.
Bowes, A. L.
description Several scientific missions have been proposed for a deeper exploration of planetary systems. These missions require a lot of specialized techniques in order to reach a better understanding of the dynamics involved in their planning. In order to help to get important features about each system under study, the present study proposes to use different definitions of integrals of the perturbing forces received by spacecrafts to help to find the best orbits for them. These computations present important information about the level of perturbation acting in the spacecraft due to the effects of each force considered in the system and they also help to understand the evolution of these perturbations. The system of Galilean moons is explored to test these techniques.
publishDate 2016
dc.date.none.fl_str_mv 2016-01-01
2018-11-26T15:44:20Z
2018-11-26T15:44:20Z
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 Spaceflight Mechanics 2016, Pts I-iv. San Diego: Univelt Inc, v. 158, p. 1565-1583, 2016.
1081-6003
http://hdl.handle.net/11449/159575
WOS:000403301400090
identifier_str_mv Spaceflight Mechanics 2016, Pts I-iv. San Diego: Univelt Inc, v. 158, p. 1565-1583, 2016.
1081-6003
WOS:000403301400090
url http://hdl.handle.net/11449/159575
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv Spaceflight Mechanics 2016, Pts I-iv
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv 1565-1583
dc.publisher.none.fl_str_mv Univelt Inc
publisher.none.fl_str_mv Univelt Inc
dc.source.none.fl_str_mv Web of Science
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
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