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1. Identity statement
Reference TypeJournal Article
Sitemtc-m16d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP7W/3E9Q9K2
Repositorysid.inpe.br/mtc-m19/2013/06.12.01.40.48   (restricted access)
Last Update2013:07.16.17.51.22 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m19/2013/06.12.01.40.49
Metadata Last Update2021:02.11.18.10.31 (UTC) administrator
DOI10.1155/2013/530516
ISSN1024-123X
Labelisi
Citation KeyChiaradiaKugaPrad:2013:OnReAr
TitleOnboard and Real-Time Artificial Satellite Orbit Determination Using GPS
Year2013
Access Date2024, May 18
Secondary TypePRE PI
Number of Files1
Size2532 KiB
2. Context
Author1 Chiaradia, Ana Paula Marins
2 Kuga, Helio Koiti
3 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JHC9
3 8JMKD3MGP5W/3C9JGJA
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 UNESP, Grp Dinam Orbital & Planetol, FEG, BR-12516410 Guaratingueta, SP, Brazil.
2 INPE, Div Space Mech & Control, BR-12227010 Sao Jose Dos Campos, SP, Brazil.
3 INPE, Div Space Mech & Control, BR-12227010 Sao Jose Dos Campos, SP, Brazil.
e-Mail Addressmarcelo.pazos@inpe.br
JournalMathematical Problems in Engineering
Volumex
NumberID 530516
History (UTC)2021-02-11 18:10:31 :: administrator -> marcelo.pazos@inpe.br :: 2013
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractAn algorithm for real-time and onboard orbit determination applying the Extended Kalman Filter (EKF) method is developed. Aiming at a very simple and still fairly accurate orbit determination, an analysis is performed to ascertain an adequacy of modeling complexity versus accuracy. The minimum set of to-be-estimated states to reach the level of accuracy of tens of meters is found to have at least the position, velocity, and user clock offset components. The dynamical model is assessed through several tests, covering force model, numerical integration scheme and step size, and simplified variational equations. The measurement model includes only relevant effects to the order of meters. The EKF method is chosen to be the simplest real-time estimation algorithm with adequate tuning of its parameters. In the developed procedure, the obtained position and velocity errors along a day vary from 15 to 20 m and from 0.014 to 0.018 m/s, respectively, with standard deviation from 6 to 10 m and from 0.006 to 0.008 m/s, respectively, with the SA either on or off. The results, as well as analysis of the final adopted models used, are presented in this work.
AreaETES
Arrangementurlib.net > Produção anterior à 2021 > DIDMC > Onboard and Real-Time...
doc Directory Contentaccess
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4. Conditions of access and use
Languageen
Target File530516.pdf
User Groupadministrator
marcelo.pazos@inpe.br
Reader Groupadministrator
marcelo.pazos@inpe.br
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryiconet.com.br/banon/2006/11.26.21.31
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.49.46 1
sid.inpe.br/bibdigital/2021/02.11.18.06 1
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m19@80/2009/08.21.17.02
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel electronicmailaddress format isbn keywords lineage mark month nextedition notes orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url
7. Description control
e-Mail (login)marcelo.pazos@inpe.br
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