| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3Jpa |
| Repository | sid.inpe.br/iris@1905/2005/08.04.01.41 (restricted access) |
| Last Update | 2019:01.16.16.07.23 (UTC) simone |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.01.41.26 |
| Metadata Last Update | 2021:02.11.18.10.05 (UTC) administrator |
| Secondary Key | INPE-9525-PRE/5178 |
| Label | 10438 |
| Citation Key | SilvaMoraKuga:2002:OrDeGP |
| Title | Orbit determination with GPS using recursive least squares method with givens rotations  |
| Format | ISBN 85-17-00006-4 |
| Year | 2002 |
| Secondary Date | 20021213 |
| Access Date | 2024, May 08 |
| Secondary Type | PRE LN |
| Number of Files | 1 |
| Size | 2783 KiB |
| 2. Context | |
| Author | 1 Silva, Aurea Aparecida da 2 Moraes, Rodolpho Vilhena de 3 Kuga, Hélio Koiti |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Winter, Othon Cabo Prado, Antonio Fernando Bertachini de Almeida. |
| Book Title | Advances in space dynamics 3: applications in astronautics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 122-131 |
| Series Title | Advances in space dynamics 3: applications in astronautics |
| History (UTC) | 2008-06-09 21:40:37 :: administrator -> jefferson :: 2012-08-02 17:54:58 :: jefferson -> administrator :: 2019-01-16 16:06:42 :: administrator -> simone :: 2002 2019-01-16 16:07:24 :: simone -> administrator :: 2002 2021-02-11 18:10:05 :: administrator -> :: 2002 |
| 3. Content and structure | |
| Is the master or a copy? | is the master |
| Content Stage | completed |
| Transferable | 1 |
| Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL orbit determination Global Positioning System GPS Pseudoranges recursive least squares method |
| Abstract | In this paper, we discuss a method of orbit determination for an artificial satellite based on the signals of the GPS constellation. The Global Positioning System is a powerful and low cost process to compute orbits for some artificial Earth satellites. This work presents a method of orbit determination for satellites with an onboard GPS receiver. Pseudoranges are used in the measurement equations for the, orbit estimator. The estimator considered is the recursive least squares method, numerically improved with orthogonal Givens rotations and dos avoiding problems; concerning inversion of matrices. Up to high order geopotential perturbations are taken into account. Preliminary results indicate that precision better than 10m is easily obtained using batches of one orbital period for the, TOPEX satellite (two hours of orbital period). Standard deviation of about 5m resulted for the residuals of pseudo-range measurements. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Orbit determination with... |
| doc Directory Content | access |
| source Directory Content | there are no files |
| agreement Directory Content | there are no files |
| 4. Conditions of access and use | |
| Target File | INPE-9525.pdf |
| User Group | administrator |
| Visibility | shown |
| Read Permission | deny from all and allow from 150.163 |
| Update Permission | not transferred |
| 5. Allied materials | |
| Next Higher Units | 8JMKD3MGPCW/446AF4B |
| Host Collection | sid.inpe.br/banon/2001/04.03.15.36 |
| 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 |