1. Identity statement | |
Reference Type | Book Section |
Site | marte3.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZ3r59YCT/GUKx8 |
Repository | sid.inpe.br/iris@1905/2005/07.29.22.31 (restricted access) |
Last Update | 2015:11.18.11.59.56 (UTC) marciana |
Metadata Repository | sid.inpe.br/iris@1905/2005/07.29.22.31.24 |
Metadata Last Update | 2021:02.11.18.09.42 (UTC) administrator |
Secondary Key | INPE-8052-PRE/3868 |
Label | 8985 |
Citation Key | ChiaradiaKugaPrad:2000:InSiGP |
Title | Investigation of the signal GPS ionospheric correction |
Format | ISBN:85-901487-1-8 |
Year | 2000 |
Secondary Date | 20010416 |
Access Date | 2024, May 08 |
Secondary Type | PRE LN |
Number of Files | 1 |
Size | 40 KiB |
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2. Context | |
Author | 1 Chiaradia, Ana Paula Marins 2 Kuga, Hélio Koiti 3 Prado, Antonio Fernando Bertachini de Almeida |
Group | 1 DMC-INPE-MCT-BR |
Editor | Prado, Antonio Fernando Bertachini de Almeida. |
Book Title | Colóquio Brasileiro de Dinâmica Orbital, 9 Advances in Space Dynamics |
Publisher | INPE |
City | São José dos Campos |
Pages | 214-218 |
Series Title | Advances in Space Dynamics |
History (UTC) | 2014-09-29 15:08:58 :: administrator -> marciana :: 2000 2015-11-18 11:59:56 :: marciana -> administrator :: 2000 2021-02-11 18:09:42 :: administrator -> :: 2000 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL astrodinâmica trajetórias espaciais mecânica celeste manobras orbitais sistema de posicionamento global astrodynamics spececraft trajectories celestial mechanics orbital maneuvers global position systems position GPS |
Abstract | The purpose of this work is to investigate a proper model to correct the ionospheric effect using single frequency GPS measurements, 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. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Investigation of the... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | there are no files |
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4. Conditions of access and use | |
Target File | 2000_chiaradia2.pdf |
User Group | administrator |
Visibility | shown |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/446AF4B |
Host Collection | sid.inpe.br/banon/2001/04.03.15.36 |
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6. Notes | |
Empty Fields | affiliation archivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume |
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