1. Identity statement | |
Reference Type | Journal Article |
Site | mtc-m16b.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZGivnK2Y/SiHdi |
Repository | sid.inpe.br/mtc-m17@80/2007/11.29.19.16 (restricted access) |
Last Update | 2007:11.29.19.19.59 (UTC) marciana |
Metadata Repository | sid.inpe.br/mtc-m17@80/2007/11.29.19.16.04 |
Metadata Last Update | 2021:02.11.18.12.07 (UTC) administrator |
Secondary Key | INPE--PRE/ |
DOI | 10.1155/2007/49781 |
ISSN | 1024-123X 1563-5147 |
Citation Key | MoraesSilvKuga:2007:SiOrDe |
Title | Simple Orbit Determination Using GPS Based on a Least-Squares Algorithm Employing Sequential Givens Rotations |
Year | 2007 |
Access Date | 2024, May 18 |
Secondary Type | PRE PI |
Number of Files | 1 |
Size | 377 KiB |
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2. Context | |
Author | 1 Moraes, Rodolpho Vilhena de 2 Silva, Aurea Aparecida da 3 Kuga, Helio Koiti |
Resume Identifier | 1 2 3 8JMKD3MGP5W/3C9JHC9 |
Group | 1 2 DMC-INPE-MCT-BR 3 DMC-INPE-MCT-BR |
Affiliation | 1 Departamento de Matemática, UNESP Campus de Guaratinguetá, Guaratinguetá 12516-410, SP, Brazil 2 Instituto Nacional de Pesquisas Espaciais (INPE) 3 Instituto Nacional de Pesquisas Espaciais (INPE) |
Journal | Mathematical Problems in Engineering |
Volume | Article ID 49781 |
History (UTC) | 2007-11-29 19:19:59 :: marciana -> administrator :: 2010-05-11 02:12:02 :: administrator -> marciana :: 2011-05-29 09:55:55 :: marciana -> administrator :: 2007 2014-08-19 19:20:48 :: administrator -> marciana :: 2007 2014-08-19 19:21:24 :: marciana -> administrator :: 2007 2021-02-11 18:12:07 :: administrator -> marciana :: 2007 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Content Type | External Contribution |
Version Type | publisher |
Abstract | A low-cost computer procedure to determine the orbit of an artificial satellite by using short arc data from an onboard GPS receiver is proposed. Pseudoranges are used as measurements to estimate the orbit via recursive least squares method. The algorithm applies orthogonal Givens rotations for solving recursive and sequential orbit determination problems. To assess the procedure, it was applied to the TOPEX/POSEIDON satellite for data batches of one orbital period (approximately two hours), and force modelling, due to the full JGM-2 gravity field model, was considered. When compared with the reference Precision Orbit Ephemeris (POE) of JPL/NASA, the results have indicated that precision better than 9 m is easily obtained, even when short batches of data are used. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Simple Orbit Determination... |
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 | |
Language | en |
Target File | moraesS1024123X07497812[1].pdf |
User Group | administrator marciana |
Reader Group | administrator marciana |
Visibility | shown |
Archiving Policy | denypublisher allowfinaldraft |
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 |
Citing Item List | sid.inpe.br/mtc-m21/2012/07.13.14.49.46 1 |
Dissemination | WEBSCI; PORTALCAPES; COMPENDEX. |
Host Collection | lcp.inpe.br/ignes/2004/02.12.18.39 cptec.inpe.br/walmeida/2003/04.25.17.12 |
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6. Notes | |
Empty Fields | alternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress electronicmailaddress format isbn keywords label lineage mark mirrorrepository month nextedition notes number orcid pages parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarymark session shorttitle sponsor subject tertiarymark tertiarytype typeofwork url |
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7. Description control | |
e-Mail (login) | marciana |
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