Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses
Autor(a) principal: | |
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Data de Publicação: | 2023 |
Outros Autores: | , , , , , , , , , |
Tipo de documento: | Artigo |
Idioma: | eng |
Título da fonte: | Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) |
Texto Completo: | http://hdl.handle.net/10773/37881 |
Resumo: | In this work, we performed a dynamical analysis of a spacecraft around a nearly equal-mass binary near-Earth asteroid with application to the asteroid 2017 YE5, which is also a possible dormant Jupiter-family comet. Thus, we investigated the motion of a particle around this binary system using the circular restricted three-body problem. We calculated the locations of the Lagrangian points of the system and their Jacobi constant. Through numerical simulations, using the Poincaré Surface of Sections, it was possible to find several prograde and retrograde periodic orbits around each binary system's primary, some exhibiting significantly-sized higher-order behavior. We also calculated the stability of these orbits. After finding the periodic orbits, we investigated the influence of solar radiation pressure on these orbits. For this analysis, we considered that the area-to-mass ratio equals 0.01 and 0.1. We also performed a spacecraft lifetime analysis considering the physical and orbital characteristics of the 2017YE5 system and investigated the behavior of a spacecraft in the vicinity of this system. We analyzed direct and retrograde orbits for different values of Jacobi's constant. This study investigated orbits that survive for at least six months, not colliding or escaping the system during that time. We also analyze the initial conditions that cause the spacecraft to collide with M1 or M2, or escape from the system. In this work, we take into account the gravitational forces of the binary asteroid system and the solar radiation pressure (SRP). Finally, we calculated optimal bi-impulsive orbital maneuvers between the collinear Lagrangian points. We found a family of possible orbital transfers considering times of flight between 0.1 and 1 day. |
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Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal massesAstrodynamicsPeriodic orbitsDouble asteroidSpace missionsIn this work, we performed a dynamical analysis of a spacecraft around a nearly equal-mass binary near-Earth asteroid with application to the asteroid 2017 YE5, which is also a possible dormant Jupiter-family comet. Thus, we investigated the motion of a particle around this binary system using the circular restricted three-body problem. We calculated the locations of the Lagrangian points of the system and their Jacobi constant. Through numerical simulations, using the Poincaré Surface of Sections, it was possible to find several prograde and retrograde periodic orbits around each binary system's primary, some exhibiting significantly-sized higher-order behavior. We also calculated the stability of these orbits. After finding the periodic orbits, we investigated the influence of solar radiation pressure on these orbits. For this analysis, we considered that the area-to-mass ratio equals 0.01 and 0.1. We also performed a spacecraft lifetime analysis considering the physical and orbital characteristics of the 2017YE5 system and investigated the behavior of a spacecraft in the vicinity of this system. We analyzed direct and retrograde orbits for different values of Jacobi's constant. This study investigated orbits that survive for at least six months, not colliding or escaping the system during that time. We also analyze the initial conditions that cause the spacecraft to collide with M1 or M2, or escape from the system. In this work, we take into account the gravitational forces of the binary asteroid system and the solar radiation pressure (SRP). Finally, we calculated optimal bi-impulsive orbital maneuvers between the collinear Lagrangian points. We found a family of possible orbital transfers considering times of flight between 0.1 and 1 day.Elsevier2025-05-19T00:00:00Z2023-05-19T00:00:00Z2023-05-19info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttp://hdl.handle.net/10773/37881eng0032-063310.1016/j.pss.2023.105701Santos, L.B.T.Sousa-Silva, P.A.Terra, M.O.Aljbaae, S.Sanchez, D.M.Prado, A.F.B.A.Oliveira, G.M.Monteiro, F.de Almeida Jr, A.K.Lima, N.B.Lima, N.B.D.info:eu-repo/semantics/embargoedAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2024-02-22T12:13:58Zoai:ria.ua.pt:10773/37881Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-20T03:08:26.478365Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse |
dc.title.none.fl_str_mv |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
title |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
spellingShingle |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses Santos, L.B.T. Astrodynamics Periodic orbits Double asteroid Space missions |
title_short |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
title_full |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
title_fullStr |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
title_full_unstemmed |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
title_sort |
Analysis of the dynamics of a spacecraft in the vicinity of an asteroid binary system with equal masses |
author |
Santos, L.B.T. |
author_facet |
Santos, L.B.T. Sousa-Silva, P.A. Terra, M.O. Aljbaae, S. Sanchez, D.M. Prado, A.F.B.A. Oliveira, G.M. Monteiro, F. de Almeida Jr, A.K. Lima, N.B. Lima, N.B.D. |
author_role |
author |
author2 |
Sousa-Silva, P.A. Terra, M.O. Aljbaae, S. Sanchez, D.M. Prado, A.F.B.A. Oliveira, G.M. Monteiro, F. de Almeida Jr, A.K. Lima, N.B. Lima, N.B.D. |
author2_role |
author author author author author author author author author author |
dc.contributor.author.fl_str_mv |
Santos, L.B.T. Sousa-Silva, P.A. Terra, M.O. Aljbaae, S. Sanchez, D.M. Prado, A.F.B.A. Oliveira, G.M. Monteiro, F. de Almeida Jr, A.K. Lima, N.B. Lima, N.B.D. |
dc.subject.por.fl_str_mv |
Astrodynamics Periodic orbits Double asteroid Space missions |
topic |
Astrodynamics Periodic orbits Double asteroid Space missions |
description |
In this work, we performed a dynamical analysis of a spacecraft around a nearly equal-mass binary near-Earth asteroid with application to the asteroid 2017 YE5, which is also a possible dormant Jupiter-family comet. Thus, we investigated the motion of a particle around this binary system using the circular restricted three-body problem. We calculated the locations of the Lagrangian points of the system and their Jacobi constant. Through numerical simulations, using the Poincaré Surface of Sections, it was possible to find several prograde and retrograde periodic orbits around each binary system's primary, some exhibiting significantly-sized higher-order behavior. We also calculated the stability of these orbits. After finding the periodic orbits, we investigated the influence of solar radiation pressure on these orbits. For this analysis, we considered that the area-to-mass ratio equals 0.01 and 0.1. We also performed a spacecraft lifetime analysis considering the physical and orbital characteristics of the 2017YE5 system and investigated the behavior of a spacecraft in the vicinity of this system. We analyzed direct and retrograde orbits for different values of Jacobi's constant. This study investigated orbits that survive for at least six months, not colliding or escaping the system during that time. We also analyze the initial conditions that cause the spacecraft to collide with M1 or M2, or escape from the system. In this work, we take into account the gravitational forces of the binary asteroid system and the solar radiation pressure (SRP). Finally, we calculated optimal bi-impulsive orbital maneuvers between the collinear Lagrangian points. We found a family of possible orbital transfers considering times of flight between 0.1 and 1 day. |
publishDate |
2023 |
dc.date.none.fl_str_mv |
2023-05-19T00:00:00Z 2023-05-19 2025-05-19T00:00:00Z |
dc.type.status.fl_str_mv |
info:eu-repo/semantics/publishedVersion |
dc.type.driver.fl_str_mv |
info:eu-repo/semantics/article |
format |
article |
status_str |
publishedVersion |
dc.identifier.uri.fl_str_mv |
http://hdl.handle.net/10773/37881 |
url |
http://hdl.handle.net/10773/37881 |
dc.language.iso.fl_str_mv |
eng |
language |
eng |
dc.relation.none.fl_str_mv |
0032-0633 10.1016/j.pss.2023.105701 |
dc.rights.driver.fl_str_mv |
info:eu-repo/semantics/embargoedAccess |
eu_rights_str_mv |
embargoedAccess |
dc.format.none.fl_str_mv |
application/pdf |
dc.publisher.none.fl_str_mv |
Elsevier |
publisher.none.fl_str_mv |
Elsevier |
dc.source.none.fl_str_mv |
reponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação instacron:RCAAP |
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Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação |
instacron_str |
RCAAP |
institution |
RCAAP |
reponame_str |
Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) |
collection |
Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) |
repository.name.fl_str_mv |
Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação |
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1799137737073229824 |