| 1. Identificação | |
| Tipo de Referência | Capítulo de Livro (Book Section) |
| Site | marte3.sid.inpe.br |
| Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identificador | 6qtX3pFwXQZ3r59YCT/H3K58 |
| Repositório | sid.inpe.br/iris@1905/2005/08.04.02.11 (acesso restrito) |
| Última Atualização | 2019:01.18.16.44.01 (UTC) simone |
| Repositório de Metadados | sid.inpe.br/iris@1905/2005/08.04.02.11.27 |
| Última Atualização dos Metadados | 2021:02.03.17.56.01 (UTC) administrator |
| Chave Secundária | INPE-9542-PRE/5195 |
| Rótulo | 10470 |
| Chave de Citação | Macau:2002:UsCoCh |
| Título | Using control of chaos to control orbita motion in a hill problem  |
| Formato | ISBN 85-17-00005-6 |
| Ano | 2002 |
| Data Secundária | 20021213 |
| Data de Acesso | 29 abr. 2024 |
| Tipo Secundário | PRE LN |
| Número de Arquivos | 1 |
| Tamanho | 3624 KiB |
| 2. Contextualização | |
| Autor | Macau, Elbert Einstein Neher |
| Grupo | LIT-INPE-MCT-BR |
| Editor | Winter, Othon Cabo Prado, Antonio Fernando Bertachini de Almeida. |
| Título do Livro | Advances in space dynamics 2: applications in astronomy |
| Editora (Publisher) | INPE |
| Cidade | São José dos Campos |
| Páginas | 251-262 |
| Título da Série | Advances in space dynamics 2: applications in astronomy |
| Histórico (UTC) | 2008-06-09 21:41:19 :: administrator -> jefferson :: 2012-08-02 17:55:11 :: jefferson -> administrator :: 2019-01-18 16:42:25 :: administrator -> simone :: 2002 2019-01-18 16:44:02 :: simone -> administrator :: 2002 2021-02-03 17:56:01 :: administrator -> :: 2002 |
| 3. Conteúdo e estrutura | |
| É a matriz ou uma cópia? | é a matriz |
| Estágio do Conteúdo | concluido |
| Transferível | 1 |
| Palavras-Chave | ENGENHARIA E TECNOLOGIA ESPACIAL chaos control orbits hill method |
| Resumo | The sensitive dependence on initial condition, which is the hallmark of chaos, has been exploited both theoretically and experimentally in the guidance of spacecraft. In general, chaos in a physical system implies accessibility to a wide range of system behaviors without requiring large perturbation. Thus, a chaotic trajectory can be used to accomplish interplanetary transfer operations expending very small amount of fuel. Besides the property of "sensitive dependence on initial condition, a chaotic invariant set has a dense set of unstable periodic orbits embedded in it. The well-known chaos control techniques use these orbits to stabilize chaotic trajectories. The purpose of this work is to show that the chaos control techniques can be used to efficiently keep a spacecraft around another body performing elaborate orbits. We consider a satellite and spacecraft moving initially in coplanar and circular orbits, with slightly different radii, around heavy central planet. The spacecraft, which is the inner body, has a slightly larger angular velocity than the satellite so that, after some time, they eventually go to a situation in which the distance between them becomes sufficiently small, so that they start to interact with one another. Considering this situation, we show that chaos control technique based on the OGY method can be used to keep the spacecraft in a desired orbit about a satellite. We also analyze the results and make considerations regarding a realistic scenario of space exploration. |
| Área | ETES |
| Arranjo | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > COLIT > Using control of... |
| Conteúdo da Pasta doc | acessar |
| Conteúdo da Pasta source | não têm arquivos |
| Conteúdo da Pasta agreement | não têm arquivos |
| 4. Condições de acesso e uso | |
| Arquivo Alvo | INPE-9542.pdf |
| Grupo de Usuários | administrator |
| 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/444BQ9E |
| Acervo Hospedeiro | sid.inpe.br/banon/2001/04.03.15.36 |
| 6. Notas | |
| Campos Vazios | affiliation archivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |