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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
IdentifierJ8LNKAN8RW/3D53S6S
Repositorydpi.inpe.br/plutao/2012/11.28.17.55
Last Update2013:01.16.17.29.31 (UTC) administrator
Metadata Repositorydpi.inpe.br/plutao/2012/11.28.17.55.08
Metadata Last Update2018:06.05.00.02.10 (UTC) administrator
Secondary KeyINPE--PRE/
ISSN2236-577X
Labellattes: 8427569272485063 1 GalskiOrla:2012:AuOrCo
Citation KeyGalskiOrla:2012:AuOrCo
TitleAutonomous orbit control procedure, using a simplified GPS navigator and a new longitude phase drift prediction method, applied to the CBERS satellite
Year2012
MonthSet.
Access Date2024, May 27
Secondary TypePRE PI
Number of Files1
Size5315 KiB
2. Context
Author1 Galski, Roberto Luiz
2 Orlando, Valcir
Resume Identifier1 8JMKD3MGP5W/3C9JJ6C
2 8JMKD3MGP5W/3C9JJAL
Group1 CRC-CRC-INPE-MCTI-GOV-BR
2 CRC-CRC-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 galski@ccs.inpe.br
2 valcir@ccs.inpe.br
e-Mail Addressgalski@ccs.inpe.br
JournalJournal of Aerospace Engineering, Sciences and Applications
Volume4
Number3
Pages54-61
History (UTC)2012-11-28 23:06:32 :: lattes -> marciana :: 2012
2013-01-16 17:35:10 :: marciana -> administrator :: 2012
2018-06-05 00:02:10 :: administrator -> marciana :: 2012
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsSatellite Control
Autonomous orbit control
GPS
Autonomous navigator
Kalman Filter
AbstractThis paper presents a performance analysis of an autonomous orbit control procedure using a simplified GPS navigator (Galski et al., 2001), where the ground track drift of the satellite is estimated on-board with help of a recently developed approach (Orlando et al., 2009) that directly calculates the acceleration of the orbit ground track as a function of the solar and geomagnetic activity. The simplified navigation procedure improves the coarse geometric navigation solution provided by GPS receivers. This is done by using the GPS solutions as inputs (observations) for a real time Kalman filtering process. The orbital state vector is extended and includes the systematic error imposed to the GPS geometric solution by the changes in the set of satellites which are visible to the receiver. The simplified navigator has reduced computational cost, allowing it to be carried and executed on-board of spacecrafts. The improved outputs of this process are used in the computational implementation of an autonomous control system for the ground track drift of the spacecraft orbit. The behavior of the system is evaluated by means of orbit simulations using a CBERS-like phased remote sensing satellite. The aim of the paper is to verify if the coupled system is able to correctly calculate and perform variable size semi-major axis orbit increment maneuvers in order to keep the satellite ground track within its allowed limits (±4km).
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > COCRC > Autonomous orbit control...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
data URLhttp://plutao.sid.inpe.br/ibi/J8LNKAN8RW/3D53S6S
zipped data URLhttp://plutao.sid.inpe.br/zip/J8LNKAN8RW/3D53S6S
Languageen
Target File5-GalskiOrlando.pdf
User Groupadministrator
lattes
marciana
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/3F3PAJE
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.15.01.12 2
sid.inpe.br/bibdigital/2013/10.19.00.29 1
URL (untrusted data)http://www.aeroespacial.org.br/jaesa/editions2.html#v4n3
DisseminationPORTALCAPES
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel doi format isbn lineage mark mirrorrepository nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork
7. Description control
e-Mail (login)marciana
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