| 1. Identity statement | |
| Reference Type | Book Section |
| Site | marte3.sid.inpe.br |
| Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
| Identifier | 6qtX3pFwXQZ3r59YCT/H3JCG |
| Repository | sid.inpe.br/iris@1905/2005/08.04.01.53 (restricted access) |
| Last Update | 2015:11.19.13.37.10 (UTC) simone |
| Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.01.53.33 |
| Metadata Last Update | 2021:02.11.18.10.05 (UTC) administrator |
| Secondary Key | INPE-9526-PRE/5179 |
| Label | 10454 |
| Citation Key | FonsecaSant:2002:SAAtCo |
| Title | SACI-2 attitude control subsystem  |
| 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 | 118 KiB |
| 2. Context | |
| Author | 1 Fonseca, Ijar Milagre 2 Santos, Marcelo C |
| 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 | 197-209 |
| Series Title | Advances in space dynamics 3: applications in astronautics |
| History (UTC) | 2008-06-09 21:40:39 :: administrator -> jefferson :: 2012-08-02 17:54:59 :: jefferson -> administrator :: 2015-11-19 13:36:48 :: administrator -> simone :: 2002 2015-11-19 13:37:10 :: 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 attitude control low Earth orbit (LEO) Brazilian Scientific Satellite SACI 2 computer simulations spin stabilization |
| Abstract | This work deals with the attitude dynamics and control of the second Brazilian Scientific Satellite SACI-2. It is a low Earth orbit (LEO)micro satellite with scientific and collecting data purposes. The work- presented in this paper involves mathematical modeling and computer simulations. In a first phase the satellite mathematical model has been derived taking into account only a partially filled ring nutation damper in order to analyze the damper performance in keeping the spin axis aligned to the angular momentum vector. In a second phase the mathematical models of the Earth magnetic field, torque coils, sensors, and control laws have been included in the satellite mathematical model to analyze the attitude control efficacy. |
| Area | ETES |
| Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > SACI-2 attitude control... |
| 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 | fonseca.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 |