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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Sitemtc-m21c.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34R/3U9HMN8
Repositóriosid.inpe.br/mtc-m21c/2019/10.22.15.10
Última Atualização2019:10.22.15.10.12 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21c/2019/10.22.15.10.12
Última Atualização dos Metadados2020:01.06.11.42.23 (UTC) administrator
Chave SecundáriaINPE--PRE/
Chave de CitaçãoMacau:2019:FoDyEx
TítuloBuilding inclinated and excentric high earth orbits through small perturbations: a four-body dynamics exploration
Ano2019
Data de Acesso16 jun. 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho34 KiB
2. Contextualização
AutorMacau, Elbert Einstein Nehrer
Identificador de Curriculo8JMKD3MGP5W/3C9JGUT
GrupoLABAC-COCTE-INPE-MCTIC-GOV-BR
AfiliaçãoInstituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autorelbert.macau@inpe.br
Nome do EventoInternational Astronautical Congress, 70.; IAF Astrodynamics Symposium
Localização do EventoWashington, DC
Data21-25 Oct.
Histórico (UTC)2019-10-22 15:10:12 :: simone -> administrator ::
2020-01-06 11:42:23 :: administrator -> simone :: 2019
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
ResumoIn specific applications, such as communication missions, require orbits with large journey time between the apogee and perigee, thus remaining for long periods at a specific point in space. Normally in these cases, the final inclination, eccentricity and semimajor axis values aimed demand too much fuel consumption when conducted by the conventional transfers methods. In this work, an alternative strategy transfer is proposed. It consists of exploring and take advantage of the natural dynamics associated to the unstable orbits and sensitive dependence present in the four body problem. In this perspective, a low cost transfer starting from a low to a high and inclinated Earth orbit is built through a combination of a lunar gravity assisted maneuver and the application of judicious and small impulses to specific points of the trajectory. The method was validated in case studies carried out for a scenario composed of Sun, Earth, Moon and vehicle. The results obtained show that it is possible to obtain the desired stable orbits with a low total impulse magnitude, even in cases where conventional transfer methods are not feasible.
ÁreaCOMP
Arranjourlib.net > BDMCI > Fonds > Produção anterior à 2021 > LABAC > Building inclinated and...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreement
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4. Condições de acesso e uso
URL dos dadoshttp://mtc-m21c.sid.inpe.br/ibi/8JMKD3MGP3W34R/3U9HMN8
URL dos dados zipadoshttp://mtc-m21c.sid.inpe.br/zip/8JMKD3MGP3W34R/3U9HMN8
Idiomaen
Arquivo Alvomacau_building.pdf
Grupo de Usuáriossimone
Visibilidadeshown
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/3ESGTTP
Lista de Itens Citandosid.inpe.br/mtc-m21/2012/07.13.14.45.07 2
Acervo Hospedeirourlib.net/www/2017/11.22.19.04
6. Notas
Campos Vaziosarchivingpolicy archivist booktitle callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn keywords label lineage mark mirrorrepository nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress readergroup readpermission rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype type url versiontype volume
7. Controle da descrição
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