Close

1. Identity statement
Reference TypeBook Section
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGPDW/3CCMDBE
Repositorysid.inpe.br/mtc-m16/2012/08.01.17.17
Last Update2012:08.01.17.17.05 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m16/2012/08.01.17.17.05
Metadata Last Update2018:06.05.01.28.54 (UTC) administrator
ISBN85-901487-1-8
Citation KeyChiaradiaKugaPrad:1998:InGPSi
TitleInvestigation of the GPS Signals Ionospheric Correction
ProjectDinâmica orbital
Year1998
Access Date2024, Dec. 26
Secondary TypePRE LI
Number of Files32
Size349 KiB
2. Context
Author1 Chiaradia, Ana Paula Marins
2 Kuga, helio Koiti
3 Prado, Antonio Fernando Bertachini de Almeida
Group1 INPE-MCT-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
EditorPrado, Antonio Fernando Bertachini de Almeida
e-Mail Addresswschulz@iae.cta.br
Book TitleAdvances in space dynamics
PublisherINPE
CitySão José dos Campos
Pages393-408
History (UTC)2012-08-01 17:17:05 :: prado@dem.inpe.br -> administrator ::
2018-06-05 01:28:54 :: administrator -> prado@dem.inpe.br :: 1998
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Keywordsastrodynamics
orbital maneuvers
AbstractThe purpose of this work is to investigate a proper model to correct the ionospheric effect using single frequency GPS easurements, which it will be used in the artificial satellite orbit determination taking in account that satellite will be above 1000 km of earth's surface. When the GPS signals are transmitted from GPS satellite to receiver, they propagate through the ionosphere causing errors on the measurements which are the highest one on signal propagation. To achieve the highest possible positioning accuracies form GPS, the ionospheric errors shall be neutralized using some kind of model and/or measurement, and they have to be considered within the adjustment process. Using dual frequency GPS receivers, the ionospheric errors can be almost totally accounted for taking advantage of the ionosphere's dispersive nature. However, this work deals with real-time determination of an artificial satellite orbit with single frequency GPS receiver. So, some model of single frequency ionospheric correction must be used. Such investigation will define to which extent the ionospheric error can affect the final accuracy of the real-time determination when using the GPS constellation.
AreaETES
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 01/08/2012 14:17 1.8 KiB 
form.php 22/10/2015 07:39 0.2 KiB 
4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGPDW/3CCMDBE
zipped data URLhttp://urlib.net/zip/8JMKD3MGPDW/3CCMDBE
Languageen
Target Fileionospheric.pdf
User Groupadministrator
jefferson
prado@dem.inpe.br
Visibilityshown
Copy HolderSID/SCD
5. Allied materials
DisseminationNTRSNASA; BNDEPOSITOLEGAL.
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber contenttype copyright creatorhistory descriptionlevel documentstage doi edition electronicmailaddress format issn label lineage mark mirrorrepository nextedition nexthigherunit notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress readergroup readpermission resumeid rightsholder schedulinginformation secondarydate secondarykey secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume
7. Description control
e-Mail (login)prado@dem.inpe.br
update 


Close