| 1. Identificação | |
| Tipo de Referência | Livro ou Monografia (Book) |
| Site | marte3.sid.inpe.br |
| Código do Detentor | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identificador | 6qtX3pFwXQZ3r59YCT/H3Epr |
| Repositório | sid.inpe.br/iris@1905/2005/08.03.22.34 (acesso restrito) |
| Última Atualização | 2016:08.31.15.48.34 (UTC) tereza@sid.inpe.br |
| Repositório de Metadados | sid.inpe.br/iris@1905/2005/08.03.22.34.08 |
| Última Atualização dos Metadados | 2021:02.11.18.24.39 (UTC) administrator |
| Chave Secundária | INPE-8535-PUD/107 |
| Rótulo | 10154 |
| Chave de Citação | Sukhanov:2002:LeAs |
| Título | Lectures on astrodynamics  |
| Ano | 2002 |
| Data de Acesso | 24 abr. 2024 |
| Tipo Secundário | NTC |
| Número de Páginas | 158 |
| Número de Arquivos | 1 |
| Tamanho | 3098 KiB |
| 2. Contextualização | |
| Autor | Sukhanov, Alexander Alexandrovich |
| Grupo | DMC-INPE-MCT-BR |
| Afiliação | Instituto Nacional de Pesquisas Espaciais (INPE) |
| Endereço de e-Mail | ivone@sid.inpe.br |
| Editora (Publisher) | INPE |
| Cidade | São josé dos Campos |
| Edição | 3 |
| Histórico (UTC) | 2006-11-16 00:18:34 :: administrator -> jefferson :: 2012-09-24 13:08:05 :: jefferson -> ivone@sid.inpe.br :: 2012-09-24 13:09:37 :: ivone@sid.inpe.br -> administrator :: 2002 2012-10-21 02:20:35 :: administrator -> ivone@sid.inpe.br :: 2002 2013-01-14 19:51:00 :: ivone@sid.inpe.br -> administrator :: 2002 2016-06-04 23:05:57 :: administrator -> tereza@sid.inpe.br :: 2002 2016-08-31 15:48:34 :: tereza@sid.inpe.br -> administrator :: 2002 2021-02-11 18:24:39 :: administrator -> tereza@sid.inpe.br :: 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 Astrodynamics two-body problem Keplerian motion perturbed theory impulse maneuvers orbital maneuvers Lambert theory Autonomous navigation least square method |
| Resumo | The lectures give a basic knowledge in different areas of Astrodynamics. These class notes contain an essence of the lectures and consist of thirteen chapters. First chapter briefly describes necessary mathematics, which is used in the lectures. Second chapter introduces in the two-body problem (Keplerian motion)and considers its main properties. Third chapter studies the Keplerian motion deeper for different orbit types; equations for the calculation of different orbital parameters and the flight time are obtained in the third chapter. Fourth chapter presents another approach to the orbital parameters and flight time calculation using a universal variable. This approach makes - the equations unified for different orbit types. Fifth chapter introduces in the theory of the perturbed motion and analyzes influence of the main perturbations, both gravitational and non-gravitational ones, on the motion. The spacecraft impulsive maneuvers changing different orbital parameters are analyzed in the sixth chapter; one, two, and three-impulse maneuvers are considered there. Seventh chapter gives an advanced solution of the Lambert problem: determination of the transfer orbit between two given positions in a given time. This solution is universal, i.e. unified with respect to the orbit types and number of complete revolutions. Interplanetary transfers including the gravity assist maneuvers are considered in eighth chapter. This consideration is based on the patched-conic approach, which is described in the chapter. Ninth chapter introduces in the space navigation, i.e. orbit determination and orbital correction maneuvers. The least square method is described in the chapter. Autonomous navigation is also briefly considered in chapter 9. Tenth chapter describes an advanced method of the state transition matrix calculation. The method is based on the matrix decomposition, which allows unifying the matrix calculation with respect to the different orbit types. The state transition matrim: is widely used in Mixes areas of Astrodynamics. Eleventh chapter considers an optimization of the orbital maneuvers. The Pontryagin's maximum principle and its applications to the optimization of the spacecraft maneuvering are described in the chapter. The electric propulsion (low thrust)and some aspects of its optimization are considered in twelfth chapter. Thirteenth chapter considers a special case of the low-thrust transfer, namely a spiral transfer by means of a transversal thrust Simple formadae for the calculation of the transfer parameters are obtained in the chapter. Note that chapters 2-5 can be applied both to the natural and artificial celestial bodies, chapters 6-13 consider mostly the spacecraft motion, navigation, and maneuvering. |
| Área | ETES |
| Arranjo | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Lectures on astrodynamics |
| 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 8535 INTERNO.pdf |
| Grupo de Usuários | administrator ivone@sid.inpe.br |
| Grupo de Leitores | administrator ivone@sid.inpe.br jefferson tereza@sid.inpe.br |
| Visibilidade | shown |
| Permissão de Leitura | deny from all and allow from 150.163 |
| Permissão de Atualização | não transferida |
| 5. Fontes relacionadas | |
| Edição Anterior | sid.inpe.br/iris@1905/2005/08.04.05.14 |
| Edição Posterior | sid.inpe.br/marciana/2003/12.19.10.13 |
| Unidades Imediatamente Superiores | 8JMKD3MGPCW/446AF4B |
| Acervo Hospedeiro | sid.inpe.br/banon/2001/04.03.15.36 |
| 6. Notas | |
| Campos Vazios | archivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi editor electronicmailaddress format isbn issn language lineage mark mirrorrepository notes numberofvolumes orcid parameterlist parentrepositories previouslowerunit progress project resumeid rightsholder schedulinginformation secondarydate secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |
| 7. Controle da descrição | |
| e-Mail (login) | tereza@sid.inpe.br |
| atualizar | |