| 1. Identificação | ||||
| Tipo de Referência | Artigo em Revista Científica (Journal Article) | |||
| Site | mtc-m21d.sid.inpe.br | |||
| Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S | |||
| Identificador | 8JMKD3MGP3W34T/47NQDRP | |||
| Repositório | sid.inpe.br/mtc-m21d/2022/10.04.13.47 (acesso restrito) | |||
| Última Atualização | 2022:10.04.13.47.05 (UTC) simone | |||
| Repositório de Metadados | sid.inpe.br/mtc-m21d/2022/10.04.13.47.05 | |||
| Última Atualização dos Metadados | 2023:01.03.16.46.19 (UTC) administrator | |||
| DOI | 10.3390/sym14091789 | |||
| ISSN | 2073-8994 | |||
| Chave de Citação | AlmeidaJrMesChiGomPra:2022:SeOrMi | |||
| Título | Searching for Orbits for a Mission to the Asteroid 2001SN(263 )Considering Errors in the Physical Parameters  | |||
| Ano | 2022 | |||
| Mês | Sept. | |||
| Data de Acesso | 12 maio 2024 | |||
| Tipo de Trabalho | journal article | |||
| Tipo Secundário | PRE PI | |||
| Número de Arquivos | 1 | |||
| Tamanho | 4056 KiB | |||
| 2. Contextualização | ||||
| Autor | 1 Almeida Junior, Allan Kardec de 2 Mescolotti, Bruna Yukiko Pinheiro Masago 3 Chiaradia, Ana Paula Marins 4 Gomes, Vivian M. 5 Prado, Antonio Fernando Bertachini de Almeida | |||
| Identificador de Curriculo | 1 2 3 4 5 8JMKD3MGP5W/3C9JGJA | |||
| ORCID | 1 0000-0002-9488-4462 2 3 4 5 0000-0002-7966-3231 | |||
| Grupo | 1 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR 2 CMC-ETES-DIPGR-INPE-MCTI-GOV-BR 3 4 5 DIMEC-CGCE-INPE-MCTI-GOV-BR | |||
| Afiliação | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Universidade Estadual Paulista (UNESP) 4 Universidade Estadual Paulista (UNESP) 5 Instituto Nacional de Pesquisas Espaciais (INPE) | |||
| Endereço de e-Mail do Autor | 1 fenixcinza@yahoo.com.br 2 3 4 5 antonio.prado@inpe.br | |||
| Revista | Symmetry-Basel | |||
| Volume | 14 | |||
| Número | 9 | |||
| Páginas | e1789 | |||
| Histórico (UTC) | 2022-10-04 13:47:35 :: simone -> administrator :: 2022 2022-10-06 15:41:26 :: administrator -> simone :: 2022 2022-11-30 19:15:42 :: simone -> administrator :: 2022 2023-01-03 16:46:19 :: administrator -> simone :: 2022 | |||
| 3. Conteúdo e estrutura | ||||
| É a matriz ou uma cópia? | é a matriz | |||
| Estágio do Conteúdo | concluido | |||
| Transferível | 1 | |||
| Tipo do Conteúdo | External Contribution | |||
| Tipo de Versão | publisher | |||
| Palavras-Chave | astrodynamics asteroid 2001SN263 errors in the physical parameters observational mission Aster mission | |||
| Resumo | The main goal of this paper is to search for orbits that can be used in the Brazilian proposed Aster mission. This mission is under study and its objective is to use a spacecraft to observe the system 2001SN263, which is a triple asteroid system. With respect to the two-body problem (spacecraft and the main asteroid), the symmetries of the orbits are broken by the oblateness of the main body of the system, the solar radiation pressure, and the gravitational attraction of the two moons of the main body. Additionally, the masses of these two moons have errors associated with their predicted values, which reinforce the asymmetry and require extra effort to maintain the observational objectives of the mission. The idea is to find orbits that remain for some time observing the three bodies of that system, even if the physical parameters of the bodies are not the ones expected from observations made from the Earth. This is accomplished by studying the effects of errors in all the physical properties of the three asteroids in the trajectories described by a spacecraft that is orbiting this system. Several important and useful trajectories are found, which are the ones that can observe the desired bodies, even if the physical parameters are not the expected ones. To express our results, we built time histories of the relative distances between each of the asteroids and the spacecraft. They are used to select the trajectories according to the amount of time that we need to observe each body of the system. In this way, the first objective of this research is to search for trajectories to keep the spacecraft close to the three bodies of the system as long as possible, without requiring orbital maneuvers. The errors for the masses of the two smaller and lesser known bodies are taken into consideration, while the mass of the most massive one is assumed to be known, because it was determined with higher precision by observations. | |||
| Área | ETES | |||
| Arranjo 1 | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Searching for Orbits... | |||
| Arranjo 2 | urlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Searching for Orbits... | |||
| Conteúdo da Pasta doc | acessar | |||
| Conteúdo da Pasta source | não têm arquivos | |||
| Conteúdo da Pasta agreement |
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| 4. Condições de acesso e uso | ||||
| Idioma | en | |||
| Arquivo Alvo | symmetry-14-01789-v2.pdf | |||
| Grupo de Usuários | simone | |||
| Grupo de Leitores | administrator simone | |||
| Visibilidade | shown | |||
| Permissão de Leitura | deny from all and allow from 150.163 | |||
| Permissão de Atualização | não transferida | |||
| 5. Fontes relacionadas | ||||
| Unidades Imediatamente Superiores | 8JMKD3MGPCW/3F2UALS 8JMKD3MGPCW/46KTFK8 | |||
| Lista de Itens Citando | sid.inpe.br/bibdigital/2022/04.03.17.52 4 sid.inpe.br/bibdigital/2013/10.14.00.13 2 sid.inpe.br/mtc-m21/2012/07.13.14.40.20 1 | |||
| Divulgação | WEBSCI | |||
| Acervo Hospedeiro | urlib.net/www/2021/06.04.03.40 | |||
| 6. Notas | ||||
| Campos Vazios | alternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark mirrorrepository nextedition notes parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url | |||
| 7. Controle da descrição | ||||
| e-Mail (login) | simone | |||
| atualizar | ||||