Publicação
Periodic orbits for space-based reflectors in the circular restricted three-body problem
| Resumo: | Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq) |
|---|---|
| Autores principais: | Salazar, F. J.T. |
| Outros Autores: | McInnes, C. R.; Winter, O. C. |
| Assunto: | Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| Ano: | 2018 |
| País: | Brasil |
| Tipo de documento: | artigo |
| Tipo de acesso: | acesso aberto |
| Instituição associada: | IBICT |
| Idioma: | inglês |
| Origem: | Oasisbr |
| _version_ | 1871568726110765056 |
|---|---|
| author | Salazar, F. J.T. |
| author2 | McInnes, C. R. Winter, O. C. |
| author2_role | author author |
| author_facet | Salazar, F. J.T. McInnes, C. R. Winter, O. C. |
| author_role | author |
| country_str | BR |
| creators_json_txt | [{\"Person.name\":\"Salazar, F. J.T.\"},{\"Person.name\":\"McInnes, C. R.\"},{\"Person.name\":\"Winter, O. C.\"}] |
| datacite.creators.creator.creatorName.fl_str_mv | Salazar, F. J.T. McInnes, C. R. Winter, O. C. |
| datacite.date.Accepted.fl_str_mv | 2017-05-01T00:00:00Z |
| datacite.date.available.fl_str_mv | 2018-12-11T17:30:12Z |
| datacite.date.embargoed.fl_str_mv | 2018-12-11T17:30:12Z |
| datacite.rights.fl_str_mv | http://purl.org/coar/access_right/c_abf2 |
| datacite.subjects.subject.fl_str_mv | Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| datacite.titles.title.fl_str_mv | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| dc.creator.none.fl_str_mv | Salazar, F. J.T. McInnes, C. R. Winter, O. C. |
| dc.date.Accepted.fl_str_mv | 2017-05-01T00:00:00Z |
| dc.date.available.fl_str_mv | 2018-12-11T17:30:12Z |
| dc.date.embargoed.fl_str_mv | 2018-12-11T17:30:12Z |
| dc.description.none.fl_str_mv | Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP) Processo FAPESP: 2011/08171-3 Processo FAPESP: 2013/03233-6 Processo FAPESP: 2015/00559-3 The use of space-based orbital reflectors to increase the total insolation of the Earth has been considered with potential applications in night-side illumination, electric power generation and climate engineering. Previous studies have demonstrated that families of displaced Earth-centered and artificial halo orbits may be generated using continuous propulsion, e.g. solar sails. In this work, a three-body analysis is performed by using the circular restricted three body problem, such that, the space mirror attitude reflects sunlight in the direction of Earth’s center, increasing the total insolation. Using the Lindstedt–Poincaré and differential corrector methods, a family of halo orbits at artificial Sun–Earth L 2 points are found. It is shown that the third order approximation does not yield real solutions after the reflector acceleration exceeds 0.245 mm s - 2, i.e. the analytical expressions for the in- and out-of-plane amplitudes yield imaginary values. Thus, a larger solar reflector acceleration is required to obtain periodic orbits closer to the Earth. Derived using a two-body approach and applying the differential corrector method, a family of displaced periodic orbits close to the Earth are therefore found, with a solar reflector acceleration of 2.686 mm s - 2. |
| dc.format.none.fl_str_mv | 95-113 |
| dc.identifier.none.fl_str_mv | http://hdl.handle.net/11449/178420 |
| dc.language.none.fl_str_mv | eng |
| dc.rights.none.fl_str_mv | http://purl.org/coar/access_right/c_abf2 |
| dc.source.none.fl_str_mv | reponame:Repositório Institucional da UNESP instname:Universidade Estadual Paulista (UNESP) instacron:UNESP |
| dc.subject.none.fl_str_mv | Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| dc.title.fl_str_mv | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| dc.type.none.fl_str_mv | http://purl.org/coar/resource_type/c_6501 |
| description | Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq) |
| dirty | 0 |
| eu_rights_str_mv | openAccess |
| format | article |
| id | oasisbr_39fba7bafa9d127037475a9edbdf4cc8 |
| identifier.url.fl_str_mv | http://hdl.handle.net/11449/178420 |
| inst_facet_str | urn:organizationAcronym:oasisbr{{{_:::_}}}IBICT |
| instacron_str | OASISBR |
| institution | IBICT |
| instname_str | IBICT |
| language | eng |
| network_acronym_str | oasisbr |
| network_name_str | Oasisbr |
| oai_identifier_str | oai:repositorio.unesp.br:11449/178420 |
| organization_str_mv | urn:organizationAcronym:oasisbr |
| person_str_mv | Salazar, F. J.T. McInnes, C. R. Winter, O. C. |
| publishDate | 2018 |
| repo_facet_str | urn:repositoryAcronym:oasisbr{{{_:::_}}}Oasisbr |
| reponame_str | Oasisbr |
| repository_id_str | urn:repositoryAcronym:oasisbr |
| service_str_mv | urn:repositoryAcronym:oasisbr |
| spelling | Periodic orbits for space-based reflectors in the circular restricted three-body problemSalazar, F. J.T.McInnes, C. R.Winter, O. C.Artificial libration pointDisplaced orbitEarth’s climate systemHalo orbitSpace reflectorsThree-body problemopen accesshttp://purl.org/coar/access_right/c_abf2http://hdl.handle.net/11449/178420HandleCelestial Mechanics and Dynamical Astronomy, v. 128, n. 1, p. 95-113, 2017.N/AHasVersion1572-9478N/AHasVersion0923-2958N/AHasVersion2-s2.0-84995741446N/AHasVersion2-s2.0-84995741446.pdfN/AHasVersionhttps://doi.org/http://dx.doi.org/10.1007/s10569-016-9739-3DOIhttp://hdl.handle.net/11449/178420Handlehttps://doi.org/10.1007/s10569-016-9739-3DOI2018-12-11T17:30:12Z2018-12-112017-05-01T00:00:00ZConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)Processo FAPESP: 2011/08171-3Processo FAPESP: 2013/03233-6Processo FAPESP: 2015/00559-3The use of space-based orbital reflectors to increase the total insolation of the Earth has been considered with potential applications in night-side illumination, electric power generation and climate engineering. Previous studies have demonstrated that families of displaced Earth-centered and artificial halo orbits may be generated using continuous propulsion, e.g. solar sails. In this work, a three-body analysis is performed by using the circular restricted three body problem, such that, the space mirror attitude reflects sunlight in the direction of Earth’s center, increasing the total insolation. Using the Lindstedt–Poincaré and differential corrector methods, a family of halo orbits at artificial Sun–Earth L 2 points are found. It is shown that the third order approximation does not yield real solutions after the reflector acceleration exceeds 0.245 mm s - 2, i.e. the analytical expressions for the in- and out-of-plane amplitudes yield imaginary values. Thus, a larger solar reflector acceleration is required to obtain periodic orbits closer to the Earth. Derived using a two-body approach and applying the differential corrector method, a family of displaced periodic orbits close to the Earth are therefore found, with a solar reflector acceleration of 2.686 mm s - 2.eng95-113reponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPjournal articlehttp://purl.org/coar/resource_type/c_6501literatureVoRhttp://purl.org/coar/version/c_970fb48d4fbd8a85 |
| spellingShingle | Periodic orbits for space-based reflectors in the circular restricted three-body problem Salazar, F. J.T. Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| status | SINGLETON |
| status_str | VoR |
| subject.fl_str_mv | Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| title | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| title_full | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| title_fullStr | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| title_full_unstemmed | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| title_short | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| title_sort | Periodic orbits for space-based reflectors in the circular restricted three-body problem |
| topic | Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| topic_facet | Artificial libration point Displaced orbit Earth’s climate system Halo orbit Space reflectors Three-body problem |
| url | http://hdl.handle.net/11449/178420 |
| visible | 1 |
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