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2 referências similares encontradas (inclusive a original) buscando em 17 dentre 17 Arquivos.
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1. Identificação
Tipo de ReferênciaArtigo em Evento (Conference Proceedings)
Siteplutao.sid.inpe.br
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identificador8JMKD3MGP3W/3HG7BP6
Repositóriosid.inpe.br/plutao/2014/12.01.11.56.55
Última Atualização2015:02.13.15.45.04 (UTC) administrator
Repositório de Metadadossid.inpe.br/plutao/2014/12.01.11.56.56
Última Atualização dos Metadados2021:02.11.18.16.34 (UTC) administrator
Rótulolattes: 1786255724025154 1 KugaCarrGagg:2014:IMDRMO
Chave de CitaçãoKugaCarrGagg:2014:ImDrMo
TítuloAn improved drag model for cbers orbit determination and propagation
FormatoDVD
Ano2014
Data de Acesso26 abr. 2024
Tipo SecundárioPRE CI
Número de Arquivos1
Tamanho362 KiB
2. Contextualização
Autor1 Kuga, Hélio Koiti
2 Carrara, Valdemir
3 Gagg, Luiz Arthur
Identificador de Curriculo1 8JMKD3MGP5W/3C9JHC9
2 8JMKD3MGP5W/3C9JJAN
Grupo1 DMC-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
Afiliação1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Endereço de e-Mail do Autor1 helio.kuga@inpe.br
2 val@dem.inpe.br
Endereço de e-Mailmarcelo.pazos@inpe.br
Nome do EventoInternational Symposium on Space Flight Dynamics, 24 (ISSFD).
Localização do EventoLaurel
Data2014
Editora (Publisher)Johns Hopkins - Applied Physics Laboratory
Páginas1-17
Título do LivroProceedings
Tipo TerciárioPaper
Histórico (UTC)2014-12-01 12:07:59 :: lattes -> administrator :: 2014
2021-02-11 18:16:34 :: administrator -> marcelo.pazos@inpe.br :: 2014
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Tipo de Versãofinaldraft
Palavras-ChaveORBIT DETERMINATION
Satellite drag
Kinetic theory of gases
ResumoThe CBERS-2B was the latest satellite of CBERS (China-Brazil Earth Resources Satellite) series, launched in 2007, and the follower CBERS-3 will be launched in late 2013. CBERS satellites have polar sun-synchronous orbit with an altitude of 778km, crossing Equator at 10:30am in descending direction, frozen eccentricity and perigee at 90 degrees, and provides global coverage of the world every 26 days. With such characteristics its orbit, besides gravitational forces, is mainly perturbed by the atmospheric drag and solar radiation pressure, amongst others (third body attraction, tides, etc.). However drag perturbation has shown to be most difficult to model in view of the need of accuracy for long lasting predictions. The current model for orbit propagation, used by the CBERS Control Center at the National Institute for the Space Research (Brazil), considers a constant value for the drag coefficient. In fact, the drag was estimated during orbit acceptance phase, which resulted a mean value of 2.7. This model was then frozen, with little variation allowed, and it is still being used for orbit determination and propagation in the INPE´s control center. Nevertheless it is known that the atmospheric drag depends on a multitude of different parameters with several sources, in particular the Mach number, the surface temperature and accommodation coefficients. In this work it is considered a model for the drag forces on CBERS based on the kinetic theory of gases, as proposed by Schaff and Cambré (1961). The algorithm considers that the external satellite geometry is described by a boundary representation (b-reps) similar to that used in computer graphics such as OpenGL software pakage. Satellite surface is divided in a finite number of triangles, each one described by its vertex coordinates. Geometry is stored in an ASCII file using a subset of NASTRAN commands for the mesh description. Once the mesh is stored in memory, the forces and torques acting on the satellite (e.g. drag and / or solar radiation pressure) can be calculated by integrating it all over the external surface. The computation burden for computing drag forces with this approach is, of course, several times higher than the constant coefficient model. The main goal of this work is to compare this model with the quasi-constant drag coefficient results from the control center, in a long term basis, for instance one month at least (between maneuvers). Therefore it is able to retrieve eventual discrepancies and the orbit elements deviation can be promptly analyzed. The atmospheric properties were obtained from an analytical model proposed by Mueller (Mueller, 1982), based on the Jacchias 1977 model (Jacchia, 1977). Indeed any density model could be used as reference to draw the essential conclusions. The results have shown that there were some significant improvements in orbit prediction, when applied for long arcs (e.g. one month). Since computing time is not a very constraining requirement nowadays, it is expected that either the variable drag coefficient on-line computation or a corresponding suitable empirical parameterization (e.g. Ziebart, 2005) can be successfully applied in the upcoming CBERS missions.
ÁreaETES
Arranjourlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > An improved drag...
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4. Condições de acesso e uso
URL dos dadoshttp://urlib.net/ibi/8JMKD3MGP3W/3HG7BP6
URL dos dados zipadoshttp://urlib.net/zip/8JMKD3MGP3W/3HG7BP6
Idiomaen
Grupo de Usuárioslattes
marcelo.pazos@inpe.br
Grupo de Leitoresadministrator
marcelo.pazos@inpe.br
Visibilidadeshown
Permissão de Leituraallow from all
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
VinculaçãoTrabalho não Vinculado à Tese/Dissertação
Repositório Espelhoiconet.com.br/banon/2006/11.26.21.31
Unidades Imediatamente Superiores8JMKD3MGPCW/446AF4B
URL (dados não confiáveis)https://dnnpro.outer.jhuapl.edu/Portals/35/ISSFD24_Paper_Release/ISSFD24_Paper_S8-4_kuga.pdf
Acervo Hospedeirodpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notas
NotasSetores de Atividade: Pesquisa e desenvolvimento científico.
Campos Vaziosarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi edition editor isbn issn lineage mark nextedition numberofvolumes orcid organization parameterlist parentrepositories previousedition previouslowerunit progress project publisheraddress rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor session shorttitle sponsor subject targetfile type volume
7. Controle da descrição
e-Mail (login)marcelo.pazos@inpe.br
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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/44N8JFH
Repositóriosid.inpe.br/mtc-m21c/2021/05.20.17.49
Última Atualização2021:05.20.17.49.21 (UTC) simone
Repositório de Metadadossid.inpe.br/mtc-m21c/2021/05.20.17.49.21
Última Atualização dos Metadados2022:04.03.19.24.43 (UTC) administrator
DOI10.5194/angeo-39-397-2021
ISSN0992-7689
Chave de CitaçãoNwankwoDCAFARCEA:2021:AtDrEf
TítuloAtmospheric drag effects on modelled low Earth orbit (LEO) satellites during the July 2000 Bastille Day event in contrast to an interval of geomagnetically quiet conditions
Ano2021
MêsMay
Data de Acesso26 abr. 2024
Tipo de Trabalhojournal article
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho3230 KiB
2. Contextualização
Autor 1 Nwankwo, Victor U. J.
 2 Denig, William
 3 Chakrabarti, Sandip K.
 4 Ajakaiye, Muyiwa P.
 5 Fatokun, Johnson
 6 Akanni, Adeniyi W.
 7 Raulin, Jean Pierre
 8 Correia, Emilia
 9 Enoh, John E.
10 Anekwe, Paul I.
Identificador de Curriculo 1
 2
 3
 4
 5
 6
 7
 8 8JMKD3MGP5W/3C9JH2C
Grupo 1
 2
 3
 4
 5
 6
 7
 8 DICEP-CGCE-INPE-MCTI-GOV-BR
Afiliação 1 Anchor University
 2 St. Joseph’s College of Maine
 3 Indian Centre for Space Physics
 4 Anchor University
 5 Anchor University
 6 Anchor University
 7 Universidade Presbiteriana Mackenzie
 8 Instituto Nacional de Pesquisas Espaciais (INPE)
 9 Interorbital systems
10 Anchor University
Endereço de e-Mail do Autor 1
 2
 3
 4
 5
 6
 7
 8 emilia.correia@inpe.br
RevistaAnnales Geophysicae
Volume39
Número3
Páginas397-412
Nota SecundáriaA2_INTERDISCIPLINAR A2_GEOCIÊNCIAS A2_ENGENHARIAS_I B2_CIÊNCIAS_BIOLÓGICAS_I B2_ASTRONOMIA_/_FÍSICA
Histórico (UTC)2021-05-20 17:49:21 :: simone -> administrator ::
2021-05-20 17:49:23 :: administrator -> simone :: 2021
2021-05-20 17:51:19 :: simone -> administrator :: 2021
2022-04-03 19:24:43 :: administrator -> simone :: 2021
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Tipo de Versãopublisher
ResumoIn this work, we simulated the atmospheric drag effect on two model SmallSats (small satellites) in low Earth orbit (LEO) with different ballistic coefficients during 1-month intervals of solar-geomagnetic quiet and perturbed conditions. The goal of this effort was to quantify how solar-geomagnetic activity influences atmospheric drag and perturbs satellite orbits, with particular emphasis on the Bastille Day event. Atmospheric drag compromises satellite operations due to increased ephemeris errors, attitude positional uncertainties and premature satellite re-entry. During a 1-month interval of generally quiescent solar-geomagnetic activity (July 2006), the decay in altitude (h) was a modest 0.53 km (0.66 km) for the satellite with the smaller (larger) ballistic coefficient of 2.2×10-3 m2 kg-1 (3.03×10-3 m2 kg-1). The associated orbital decay rates (ODRs) during this quiet interval ranged from 13 to 23m per day (from 16 to 29m per day). For the disturbed interval of July 2000 the significantly increased altitude loss and range of ODRs were 2.77 km (3.09 km) and 65 to 120m per day (78 to 142m per day), respectively. Within the two periods, more detailed analyses over 12 d intervals of extremely quiet and disturbed conditions revealed respective orbital decays of 0.16 km (0.20 km) and 1.14 km (1.27 km) for the satellite with the smaller (larger) ballistic coefficient. In essence, the model results show that there was a 6- to 7-fold increase in the deleterious impacts of satellite drag between the quiet and disturbed periods. We also estimated the enhanced atmospheric drag effect on the satellites' parameters caused by the July 2000 Bastille Day event (in contrast to the interval of geomagnetically quiet conditions). The additional percentage increase, due to the Bastille Day event, to the monthly mean values of h and ODR are 34.69%and 50.13% for Sat-A and 36.45% and 68.95% for Sat-B. These simulations confirmed (i) the dependence of atmospheric drag force on a satellite's ballistic coefficient, and (ii) that increased solar-geomagnetic activity substantially raises the degrading effect of satellite drag. In addition, the results indicate that the impact of short-duration geomagnetic transients (such as the Bastille Day storm) can have a further deleterious effect on normal satellite operations. Thus, this work increases the visibility and contributes to the scientific knowledge surrounding the Bastille Day event and also motivates the introduction of new indices used to describe and estimate the atmospheric drag effect when comparing regimes of varying solar-geomagnetic activity.We suggest that a model of satellite drag, when combined with a high-fidelity atmospheric specification as was done here, can lead to improved satellite ephemeris estimates.
ÁreaCEA
Arranjourlib.net > BDMCI > Fonds > Produção a partir de 2021 > CGCE > Atmospheric drag effects...
Conteúdo da Pasta docacessar
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4. Condições de acesso e uso
URL dos dadoshttp://urlib.net/ibi/8JMKD3MGP3W34R/44N8JFH
URL dos dados zipadoshttp://urlib.net/zip/8JMKD3MGP3W34R/44N8JFH
Arquivo Alvoangeo-39-397-2021.pdf
Grupo de Usuáriossimone
Grupo de Leitoresadministrator
simone
Visibilidadeshown
Política de Arquivamentoallowpublisher allowfinaldraft
Permissão de Atualizaçãonão transferida
5. Fontes relacionadas
Unidades Imediatamente Superiores8JMKD3MGPCW/46KTFK8
DivulgaçãoWEBSCI; PORTALCAPES; COMPENDEX; 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 language lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readpermission rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject tertiarymark tertiarytype url
7. Controle da descrição
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