1. Identity statement | |
Reference Type | Book Section |
Site | mtc-m21c.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 8JMKD3MGP3W34R/3SMUC5H |
Repository | sid.inpe.br/mtc-m21c/2019/02.08.17.13 (restricted access) |
Last Update | 2019:02.08.17.13.10 (UTC) simone |
Metadata Repository | sid.inpe.br/mtc-m21c/2019/02.08.17.13.10 |
Metadata Last Update | 2020:01.06.11.42.09 (UTC) administrator |
Secondary Key | INPE--/ |
DOI | 10.1007/978-3-319-99268-6_38 |
Citation Key | RomeroSouz:2019:SaCoSy |
Title | Satellite controller system based on reaction wheels using the State-Dependent Riccati Equation (SDRE) on Java |
Year | 2019 |
Access Date | 2024, May 19 |
Secondary Type | PRE LI |
Number of Files | 1 |
Size | 1492 KiB |
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2. Context | |
Author | 1 Romero, Alessandro Gerlinger 2 Souza, Luiz Carlos Gadelha de |
Resume Identifier | 1 2 8JMKD3MGP5W/3C9JHN3 |
Group | 1 CMC-ETES-SESPG-INPE-MCTIC-GOV-BR |
Affiliation | 1 Instituto Nacional de Pesquisas Espaciais (INPE) 2 Universidade Federal do ABC (UFABC) |
Author e-Mail Address | 1 romgerale@yahoo.com.br 2 luiz.gadelha@ufabc.edu.br |
Editor | Cavalca, Katia Lucchesi Weber, Hans Ingo |
Book Title | Proceedings of the 10th International Conference on Rotor Dynamics - IFToMM |
Publisher | Springer |
Pages | 547-561 |
History (UTC) | 2019-02-08 17:13:36 :: simone -> administrator :: 2019 2020-01-06 11:42:09 :: administrator -> simone :: 2019 |
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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 |
Keywords | Nonlinear control · SDRE · Satellite · Attitude Reaction wheels |
Abstract | Complex space missions involving large angle maneuvers and fast attitude control require nonlinear control methods to design the Satellite Controller System (SCS) in order to satisfy robustness and performance requirements. One candidate method for a nonlinear SCS control law is the State-Dependent Riccati Equation (SDRE). SDRE provides an effective algorithm for synthesizing nonlinear feedback control by allowing nonlinearities in the system states while offering great design flexibility through state-dependent weighting matrices. In that context, analysis by simulation of nonlinear control methods can save money and time. Although, commercial 3D simulators exist that can accommodate various satellites components including the controllers, in this paper, we present a 3D simulator and the investigation of a SDRE control law performance by simulations. The simulator is implemented based on Java and related open-source software libraries (Hipparchus - linear algebra library, and Orekit - flight dynamics library), therefore, it can run in a variety of platforms and it has low cost. These open-source libraries were extended in order to solve the optimization problem that is the cornerstone of the SDRE method, a major contribution of the simulator. The simulator is evaluated taking into account a typical mission of the Brazilian National Institute for Space Research (INPE), in which the SCS must stabilize a satellite in three-axis using reaction wheels so that the optical payload can point to the desired target. Two SCS control laws (a linear and a SDRE based) were simulated for an attitude maneuver in the launch and early orbit phase (LEOP), the upside-down maneuver. The results of simulations shown that SDRE-based controller provides better performance. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Satellite controller system... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | |
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4. Conditions of access and use | |
Language | en |
Target File | romero_satelllite.pdf |
User Group | simone |
Reader Group | administrator simone |
Visibility | shown |
Read Permission | deny from all |
Update Permission | not transferred |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/3F2UALS |
Citing Item List | sid.inpe.br/mtc-m21/2012/07.13.14.54.10 5 sid.inpe.br/bibdigital/2013/10.14.00.13 1 |
Dissemination | BNDEPOSITOLEGAL |
Host Collection | urlib.net/www/2017/11.22.19.04 |
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6. Notes | |
Empty Fields | archivingpolicy archivist callnumber city copyholder copyright creatorhistory descriptionlevel e-mailaddress edition format isbn issn label lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarymark serieseditor seriestitle session shorttitle sponsor subject tertiarymark tertiarytype translator url volume |
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7. Description control | |
e-Mail (login) | simone |
update | |
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