| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3JkH |
| Repository | sid.inpe.br/iris@1905/2005/08.04.01.38 (restricted access) |
| Last Update | 2019:01.16.16.05.01 (UTC) simone |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.01.38.20 |
| Metadata Last Update | 2021:02.11.18.10.04 (UTC) administrator |
| Secondary Key | INPE-9522-PRE/5175 |
| Label | 10435 |
| Citation Key | KugaFurl:2002:ErAnRo |
| Title | Error analysis for routine orbit determination of the French-Brazilian Micro-Satellite  |
| 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 | 2446 KiB |
| 2. Context | |
| Author | 1 Kuga, Hélio Koiti 2 Furlan, Benedito Marcio P |
| Group | 1 DMC-INPE-MCT-BR |
| Editor | Winter, Othon Cabo Prado, Antonio Fernando Bertachini de Almeida |
| Book Title | Cóloquio Brasileiro de Dinâmica Orbital, 10 Advances in space dynamics 3: applications in astronautics |
| Publisher | INPE |
| City | São José dos Campos |
| Pages | 80-87 |
| Series Title | Advances in space dynamics 3: applications in astronautics |
| History (UTC) | 2008-06-09 21:40:33 :: administrator -> jefferson :: 2012-08-02 17:54:57 :: jefferson -> administrator :: 2019-01-16 16:04:33 :: administrator -> simone :: 2002 2019-01-16 16:05:02 :: simone -> administrator :: 2002 2021-02-11 18:10:04 :: 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 French Brazilian Micro satellite mission (FBM) Doppler measuremen oscillator stability error analysis routine orbit determination |
| Abstract | The work presents de error analyses for the routine orbit determination of the, French Brazilian Micro satellite mission. The basic space and ground segment requirements impose usage of single tracking station collecting one-way Doppler measurements, with on-board oscillator stability of medium level for a nearly circular low Earth orbit. The measurement error, and errors steaming from the dynamical modeling were considered. The analysis results depict the achievable, accuracy with such a system as designed to the French Brazilian micro-satellite mission. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Error analysis for... |
| 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-9522.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 |