TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE
Autor(a) principal: | |
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Data de Publicação: | 2016 |
Outros Autores: | , , , , , , |
Tipo de documento: | Artigo de conferência |
Idioma: | eng |
Título da fonte: | Repositório Institucional da UNESP |
Texto Completo: | http://hdl.handle.net/11449/159574 |
Resumo: | The idea of the present paper is to study transfers in the restricted three-body problem considering the effects of the radiation pressure in the trajectory of the spacecraft in a bi-impulsive maneuver. Three systems of primaries are used: Sun-Earth, a generic Sun-asteroid system and a system of asteroids. Transfers among the Lagrangian points and between the Lagrangian points and the primaries are considered. The results show that the radiation pressure has a significant participation in the process, in particular in the system formed by asteroids, because their gravitational forces are smaller compared with the systems having larger bodies. In the case of the asteroid system, it is possible to find solutions with lower fuel consumption by considering the solar radiation pressure. The idea is not to use the radiation pressure as a control, but just to measure its effects when performing the bi-impulsive transfer. It is very important to consider this force or the spacecraft will not reach the desired point. |
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Repositório Institucional da UNESP |
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spelling |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSUREThe idea of the present paper is to study transfers in the restricted three-body problem considering the effects of the radiation pressure in the trajectory of the spacecraft in a bi-impulsive maneuver. Three systems of primaries are used: Sun-Earth, a generic Sun-asteroid system and a system of asteroids. Transfers among the Lagrangian points and between the Lagrangian points and the primaries are considered. The results show that the radiation pressure has a significant participation in the process, in particular in the system formed by asteroids, because their gravitational forces are smaller compared with the systems having larger bodies. In the case of the asteroid system, it is possible to find solutions with lower fuel consumption by considering the solar radiation pressure. The idea is not to use the radiation pressure as a control, but just to measure its effects when performing the bi-impulsive transfer. It is very important to consider this force or the spacecraft will not reach the desired point.Natl Inst Space Res INPE, Sao Jose Dos Campos, BrazilFed Ctr Technol Educ Minas Gerais CEFET MG, Contagem, BrazilSao Paulo State Univ, FEG UNESP, Guaratingueta, BrazilNatl Inst Space Res INPE, INPE Brazil, Board Grad Sch, Sao Jose Dos Campos, BrazilNatl Inst Space Res INPE, DMC, Sao Jose Dos Campos, BrazilPurdue Univ, Sch Aeronaut & Astronaut, 701 West Stadium Ave, W Lafayette, IN 47907 USASao Paulo State Univ, FEG UNESP, Guaratingueta, BrazilUnivelt IncNatl Inst Space Res INPEFed Ctr Technol Educ Minas Gerais CEFET MGUniversidade Estadual Paulista (Unesp)Purdue UnivOliveira, Geraldo Magela C.Gomes, Vivian M. [UNESP]Prado, Antonio F. Bertachini de A.Sanchez, Diogo M.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/conferenceObject1513-1530Spaceflight Mechanics 2016, Pts I-iv. San Diego: Univelt Inc, v. 158, p. 1513-1530, 2016.1081-6003http://hdl.handle.net/11449/159574WOS:000403301400087Web of Sciencereponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengSpaceflight Mechanics 2016, Pts I-ivinfo:eu-repo/semantics/openAccess2021-10-23T21:44:26Zoai:repositorio.unesp.br:11449/159574Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-23T21:44:26Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false |
dc.title.none.fl_str_mv |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
title |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
spellingShingle |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE Oliveira, Geraldo Magela C. |
title_short |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
title_full |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
title_fullStr |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
title_full_unstemmed |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
title_sort |
TRANSFERS BETWEEN THE LAGRANGIAN POINTS AND THE PRIMARIES CONSIDERING RADIATION PRESSURE |
author |
Oliveira, Geraldo Magela C. |
author_facet |
Oliveira, Geraldo Magela C. Gomes, Vivian M. [UNESP] Prado, Antonio F. Bertachini de A. Sanchez, Diogo M. Zanetti, R. Russell, R. P. Ozimek, M. T. Bowes, A. L. |
author_role |
author |
author2 |
Gomes, Vivian M. [UNESP] Prado, Antonio F. Bertachini de A. Sanchez, Diogo M. 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 Fed Ctr Technol Educ Minas Gerais CEFET MG Universidade Estadual Paulista (Unesp) Purdue Univ |
dc.contributor.author.fl_str_mv |
Oliveira, Geraldo Magela C. Gomes, Vivian M. [UNESP] Prado, Antonio F. Bertachini de A. Sanchez, Diogo M. Zanetti, R. Russell, R. P. Ozimek, M. T. Bowes, A. L. |
description |
The idea of the present paper is to study transfers in the restricted three-body problem considering the effects of the radiation pressure in the trajectory of the spacecraft in a bi-impulsive maneuver. Three systems of primaries are used: Sun-Earth, a generic Sun-asteroid system and a system of asteroids. Transfers among the Lagrangian points and between the Lagrangian points and the primaries are considered. The results show that the radiation pressure has a significant participation in the process, in particular in the system formed by asteroids, because their gravitational forces are smaller compared with the systems having larger bodies. In the case of the asteroid system, it is possible to find solutions with lower fuel consumption by considering the solar radiation pressure. The idea is not to use the radiation pressure as a control, but just to measure its effects when performing the bi-impulsive transfer. It is very important to consider this force or the spacecraft will not reach the desired point. |
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. 1513-1530, 2016. 1081-6003 http://hdl.handle.net/11449/159574 WOS:000403301400087 |
identifier_str_mv |
Spaceflight Mechanics 2016, Pts I-iv. San Diego: Univelt Inc, v. 158, p. 1513-1530, 2016. 1081-6003 WOS:000403301400087 |
url |
http://hdl.handle.net/11449/159574 |
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 |
1513-1530 |
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 |
|
_version_ |
1803046081565556736 |