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Reference TypeThesis
Identifier6qtX3pFwXQZ3P8SECKy/GL24r
Repositorysid.inpe.br/jeferson/2005/07.14.18.30
Metadatasid.inpe.br/jeferson/2005/07.14.18.30.23
Sitemtc-m16b.sid.inpe.br
Secondary KeyINPE-12539-TDI/1001
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Citation KeyFelipe:2004:TrOrEn
AuthorFelipe, Gislaine de
GroupSPG-INPE-MCT-BR
TitleTransferência orbitais envolvendo órbitas do tipo halo
Year2004
CommitteeMoraes, Rodolpho Vilhena de (presidente)
Prado, Antonio Fernando Bertachini de Almeida (orientador)
Winter, Othon Cabo
Chiaradia, Ana Paula Martins
Zanardi, Maria Cecília França de Paula Santos
Date2004-03-19
Alternate TitleTransfers involving orbits of type halo
UniversityInstituto Nacional de Pesquisas Espaciais (INPE)
CitySão José dos Campos
Keywordstransferência de órbitas, órbita de Rendezvous, mecânica orbital, manobra orbital, problemas de três corpos, órbitas de veículos espaciais, transfer orbits, orbital Rendezvous, orbital mechanics, orbital maneuvers, three body problems, spacecraf orbits.
AbstractNas atividades espaciais, é de grande importância o estudo das trajetórias que os veículos espaciais devem seguir para completar uma missão. No presente trabalho, estudam-se as manobras orbitais envolvendo órbitas Halo para vários sistemas de primários. Para realizar este estudo utiliza-se o método de Lindstedt-Poincaré para a determinação das órbitas e o método de Lambert para as transferências envolvidas, tanto para as transferências com tempo livre como para as manobras de rendez-vous. Para exemplificar as técnicas desenvolvidas uma missão completa no sistema Terra-Lua envolvendo o problema restrito de três corpos é calculada em detalhes. Ainda estudam-se neste trabalho as mesmas manobras para o problema restrito bi-circular de quatro corpos. A seguir, um modelo propulsado de swing-by é desenvolvido e a sua eficiência em transferir um veiculo entre uma órbita de estacionamento em tomo da Terra até uma órbita Halo no sistema Terra-Sol utilizando um swing-by coma Lua é medida. ABSTRACT: In space activities, it is of great importance the study of trajectories that the space vehicles should follow to complete a mission. In the present work, maneuvers involving Halo orbits for several systems of primary are studied. To accomplish this study the method of Lindstedt-Poincaré is used for the etermination of the orbits and the method of Lambert is used for the transfers involved in both cases for the transfers with free time for the rendez-vous maneuvers. To exemplify the techniques developed here a complete mission in the Earth-Moon system involving the restricted three bodies problem is calculated in details. It is still studied in this work the same maneuvers for the restricted bi-circular problem of four bodies. To proceed, a propelled model for the swing-by is studied and its efficiency in transfering a spacecraft from a parking orbit around the Earth to a Halo orbit in the Earth-Sun system using a swing-by with the Moon is measured.
Number of Pages222
Languagept
Thesis TypeTese (Doutorado em Mecânica Espacial e Controle)
Secondary TypeTDI
DisseminationNTRSNASA; BNDEPOSITOLEGAL.
AreaETES
CourseETE
Size3601 KiB
Number of Files1
Target Filepublicacao.pdf
Last Update2020:02.14.14.30.17 cptec.inpe.br/walmeida/2003/04.25.17.12 sergio
Metadata Last Update2020:02.14.14.31.52 cptec.inpe.br/walmeida/2003/04.25.17.12 sergio {D 2004}
Document Stagecompleted
Is the master or a copy?is the master
e-Mail (login)sergio
User Groupadministrator ivone@sid.inpe.br jefferson sergio simone
Copy HolderSID/SCD
Visibilityshown
Transferable1
Host Collectioncptec.inpe.br/walmeida/2003/04.25.17.12
Document Stagenot transferred
Secondary Date2005-06-07
Copyright Repositoryurlib.net/www/2012/11.12.15.10
Read Permissionallow from all
source Directory Content
publicacao.pdf 14/02/2020 11:31 3.5 MiB
agreement Directory Content
TERMO DE DEPOSITO ASSINADO GISLAINE DE FELIPE DOUTORADO.pdf 14/02/2020 11:30 407.3 KiB
History2005-07-14 18:31:57 :: jefferson -> jeferson ::
2005-09-20 14:29:18 :: jeferson -> jefferson ::
2007-09-05 17:05:34 :: jefferson -> administrator ::
2008-08-21 20:44:41 :: administrator -> jefferson ::
2008-11-11 17:04:27 :: jefferson -> administrator ::
2009-07-07 20:05:37 :: administrator -> jefferson ::
2012-07-18 14:58:44 :: jefferson -> ivone@sid.inpe.br ::
2012-07-18 14:59:41 :: ivone@sid.inpe.br -> administrator :: 2004
2012-10-21 21:44:29 :: administrator -> ivone@sid.inpe.br :: 2004
2013-01-14 19:46:51 :: ivone@sid.inpe.br -> administrator :: 2004
2018-06-05 03:52:25 :: administrator -> tereza@sid.inpe.br :: 2004
2019-04-01 14:32:14 :: tereza@sid.inpe.br -> simone :: 2004
2020-02-14 14:29:26 :: simone -> sergio :: 2004
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Access Date2020, Feb. 17
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