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1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Sitemtc-m21c.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W34R/42LA7DL
Repositóriosid.inpe.br/mtc-m21c/2020/06.10.15.39   (acesso restrito)
Última Atualização2020:06.10.15.39.10 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21c/2020/06.10.15.39.10
Última Atualização dos Metadados2022:01.04.01.35.12 (UTC) administrator
DOI10.1140/epjst/e2020-900161-1
ISSN1951-6355
Chave de CitaçãoCarvalhoMora:2020:SeApUs
TítuloA semi-analytical approach using the single and double averaged methods and the Lidov–Kozai mechanism
Ano2020
MêsMay
Data de Acesso05 maio 2024
Tipo de Trabalhojournal article
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho2974 KiB
2. Contextualização
Autor1 Carvalho, Jean P. S.
2 Moraes, Rodolpho Vilhena de
Grupo1
2 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Afiliação1 Universidade Federal do Recôncavo da Bahia (UFRBA)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 jeanfeg@gmail.com
RevistaEuropean Physical Journal Special Topics
Volume229
Número8
Páginas1491-1500
Histórico (UTC)2020-06-10 15:39:44 :: simone -> administrator :: 2020
2022-01-04 01:35:12 :: administrator -> simone :: 2020
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Tipo de Versãopublisher
ResumoAn analysis of the orbital motion of artificial satellites around Mercury is presented taking into account its non-sphericity (J(2), J(3), C-22) and the perturbation of the third body. The disturbing potential due to the third body is developed in circular and inclined orbit. The double-averaged method should be used with caution in some situations where the averaging is applied at different timescales. In this work, a study is presented considering this observation for orbits around Mercury. When the mean anomaly of the Sun is eliminated, the idea is that all effects whose periods below 88 days are neglected. As the rotation of Mercury is about 58.6 days, this means that the perturbation due to the C-22 term must also be neglected. However, since the C-22 term is important and should be taken into account, then terms longer than 58.6 days should also be preserved. In other words, keeping the C-22 term with a period of 58.6 days means that the solar terms with the longest period (88 days) will be maintained here. The single-averaged method is applied to eliminate only the mean anomaly of the spacecraft. A comparison between the single and double averaged models is presented. We found that for the case of Mercury the two models are in agreement, but the single-averaged model is more realistic because it keeps more terms in the disturbing potential. Several types of resonances can be analyzed starting of the single-averaged potential. Considering our single-averaged disturbing potential, the terms due to Lidov-Kozai resonance were isolated to make a qualitative analysis considering the libration and circulation regions in the diagram, eccentricity versus argument of the pericenter.
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4. Condições de acesso e uso
Idiomaen
Arquivo Alvocarvalho_semi.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Política de Arquivamentodenypublisher denyfinaldraft12
Permissão de Leituradeny from all and allow from 150.163
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
Lista de Itens Citandosid.inpe.br/bibdigital/2021/02.11.18.06 1
DivulgaçãoPORTALCAPES; SCOPUS.
Acervo Hospedeirourlib.net/www/2017/11.22.19.04
6. Notas
Campos Vaziosalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn keywords label lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project resumeid rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url
7. Controle da descrição
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