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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/37NQPT8
Repositorydpi.inpe.br/plutao@80/2010/06.25.15.01
Last Update2010:07.02.17.36.01 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao@80/2010/06.25.15.01.55
Metadata Last Update2021:02.11.18.11.20 (UTC) administrator
Secondary KeyINPE--PRE/
ISSN1991-8747
Labellattes: 1786255724025154 3 GomesPradKuga:2010:ReTiOr
Citation KeyGomesPradKuga:2010:ReTiOr
TitleReal time orbit determination with different force fields
Year2010
MonthJan.
Access Date2024, May 18
Secondary TypePRE PI
Number of Files1
Size940 KiB
2. Context
Author1 Gomes, Vivian Martins
2 Prado, Antonio F B A
3 Kuga, Helio Koiti
Resume Identifier1
2
3 8JMKD3MGP5W/3C9JHC9
Group1 DMC-ETE-INPE-MCT-BR
2 DMC-ETE-INPE-MCT-BR
3 DMC-ETE-INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 hkk@dem.inpe.br
e-Mail Addresshkk@dem.inpe.br
JournalWSEAS Transactions on Applied and Theoretical Mechanics
Volume5
Number1
Pages23-32
History (UTC)2010-06-29 12:04:19 :: lattes -> marciana :: 2010
2010-07-02 17:36:01 :: marciana -> banon :: 2010
2010-07-14 18:06:32 :: banon -> administrator :: 2010
2010-12-08 15:20:02 :: administrator -> marciana :: 2010
2011-05-20 05:56:45 :: marciana -> administrator :: 2010
2021-02-11 18:11:20 :: administrator -> marciana :: 2010
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsGeodetic satellites - Astrophysics - Global positioning system - Kalman filters - Radio navigation - Signal processing - Sun
AbstractThe Global Positioning System (GPS) is a satellite navigation system that allows the users to determine 3D positioning and the time with high precision. Its main purposes are: aid to radionavigation in three dimensions with high precision positioning, navigation in real time, time synchronization, global coverage and quick acquisition of data signal sent by the GPS satellites. In this work, it is proposed to estimate, in real time, an orbital state vector composed by position, velocity, bias and drift of the GPS receiver clock on board satellites by processing the raw navigation solution obtained by the on-board receiver. In this work the Kalman filter is used to estimate the state vector based on the stepwise incoming navigation solution from the receiver. The Kalman filter is used due to its robustness in real time applications, without unnecessary storage of observations, as they can be processed while being collected. The filter dynamic model includes perturbation due to geopotential, solar radiation pressure and perturbations due to the Sun and the Moon and the observations are the raw navigation solution composed of position and receiver clock bias. Simulations and tests are done using actual data from TOPEX/POSEIDON satellite. For performance assessment, a comparison is done between the estimated state vector and the precise orbit ephemeris (POE) produced by JPL/NASA.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Real time orbit...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://urlib.net/ibi/J8LNKAN8RW/37NQPT8
zipped data URLhttp://urlib.net/zip/J8LNKAN8RW/37NQPT8
Languageen
Target File89-141.pdf
User Groupadministrator
banon
lattes
marciana
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 2
URL (untrusted data)http://www.worldses.org/journals/mechanics/mechanics-2010.htm
DisseminationCOMPENDEX
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
NotesSetores de Atividade: Pesquisa e desenvolvimento científico.
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi format isbn lineage mark mirrorrepository nextedition orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork versiontype
7. Description control
e-Mail (login)marciana
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