Fechar

1. Identificação
Tipo de ReferênciaArtigo em Revista Científica (Journal Article)
Código do Detentorisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Sitemarte3.sid.inpe.br (namespace prefix: upn:EEU3D2)
Identificador6qtX3pFwXQZ3r59YCT/GUcQU
Repositóriosid.inpe.br/iris@1905/2005/07.28.21.48.38   (acesso restrito)
Última Atualização2018:01.02.11.23.28 (UTC) marciana
Repositório de Metadadossid.inpe.br/iris@1905/2005/07.28.21.48.41
Última Atualização dos Metadados2021:02.11.18.13.13 (UTC) administrator
Chave SecundáriaINPE-9214-PRE/4886
ISSN0273-1177
Rótulo3136
Chave de CitaçãoGillKuga:1993:ImApTo
TítuloODEM: an improved approach towards rapid satellite maneuver calibration
Formato(AAS93-111)
Ano1993
Data de Acesso24 out. 2026
Tipo SecundárioPRE PI
Número de Arquivos1
Tamanho517 KiB
2. Contextualização
Autor1 Gill, Eberhard
2 Kuga, Hélio Koiti
Grupo1 DMC-INPE-MCT-BR
RevistaAdvances in Space Research
Volume82
NúmeroPar 1/2
Páginas783-802
Acervo Hospedeirosid.inpe.br/banon/2001/04.03.15.36 upn:EEU3D2
Histórico (UTC)2008-06-09 16:22:27 :: administrator -> banon ::
2010-05-12 14:32:20 :: banon -> jefferson ::
2012-10-03 16:26:24 :: jefferson -> administrator ::
2016-06-04 23:04:15 :: administrator -> marciana :: 1993
2018-01-02 11:23:28 :: marciana -> administrator :: 1993
2021-02-11 18:13:13 :: administrator -> marciana :: 1993
3. Conteúdo e estrutura
É a matriz ou uma cópia?é a matriz
Estágio do Conteúdoconcluido
Transferível1
Tipo do ConteúdoExternal Contribution
Palavras-ChaveAPPLICATIONS PROGRAMS (COMPUTERS)
ASTRODYNAMICS
CALIBRATING GEOSYNCHRONOUS ORBITS
ORBITCALCULATION
ORBITAL MANEUVERS
ORBITAL MECHANICS
SATELLITE ORBITS
ALGORITHMS
APOGEE BOOST MOTORS
MATHEMATICAL MODELS
ROCKET THRUST
orbit determination
ResumoResulting from a cooperation program between the German Space Operations Center (GSOC) of the German Aerospace Research Establishment and the Brazilian Instituto Nacional de Pesquisas (INPE) a new general orbit determination system has recently been developed. Although the software supports orbit determination for all types of Earth satellite orbits it is especially suited to orbit determination in the course of the positioning phase of geostationary satellites. The features of the ODEM (Orbit Determination including Extended Maneuvers) software comprise the precise modeling of extended thrust phases and utilization of 3-way Doppler data which is essential for an improved orbit determination accuracy based on short tracking data arcs. The mathematical algorithms implemented to model the extended spacecraft thrust phases for different types of satellites are presented together with a brief overall software description. Extended thrust phase monitoring and estimation is particularly interesting for two main fields of application, which are analyzed using data from a recently performed positioning: Rapid diagnosis of the apogee boost maneuvers and calibration of station acquisition maneuvers. Results are presented for the achieved level of the final residuals as well as for the comparison of the estimated thrust values obtained from ODEM and conventional methods. The benefit, resulting from the processing of 3-way Doppler data, is discussed.
ÁreaETES
Arranjourlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > ODEM: an improved...
Conteúdo da Pasta docacessar
Conteúdo da Pasta sourcenão têm arquivos
Conteúdo da Pasta agreementnão têm arquivos
4. Condições de acesso e uso
Grupo de Usuáriosadministrator
banon
jefferson
Grupo de Leitoresadministrator
jefferson
marciana
Visibilidadeshown
Política de Arquivamentodenypublisher denyfinaldraft24
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 - 74
sid.inpe.br/bibdigital@80/2006/04.07.15.50.13 - 1
sid.inpe.br/banon/2001/04.03.15.36.19 - 1
DivulgaçãoWEBSCI; PORTALCAPES; MGA; COMPENDEX.
6. Notas
NotasAAS - AIAA Spaceflight Mechanics Meeting, 3, 22-24 fEB., 1993, Pasadena.
Campos Vaziosaffiliation alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress electronicmailaddress isbn language lineage mark mirrorrepository month nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project resumeid rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject targetfile tertiarymark tertiarytype typeofwork url versiontype
7. Controle da descrição
e-Mail (login)marciana
atualizar 


Fechar