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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21c.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34R/3TQ7C6P
Repositorysid.inpe.br/mtc-m21c/2019/08.07.11.05
Last Update2019:08.07.11.05.46 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21c/2019/08.07.11.05.46
Metadata Last Update2021:02.11.18.10.57 (UTC) administrator
DOI10.1117/1.JRS.13.032509
ISSN1931-3195
Citation KeyRomeroSouz:2019:StRiEq
TitleState-dependent Riccati equation controller using Java in remote sensing CubeSats
Year2019
MonthJuly
Access Date2024, May 19
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size1551 KiB
2. Context
Author1 Romero, Alessandro Gerling
2 Souza, Luiz Carlos Gadelha de
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
Group1 DIDMC-CGETE-INPE-MCTIC-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Universidade Federal do ABC (UFABC)
Author e-Mail Address1 romgerale@yahoo.com.br
JournalJournal of Applied Remote Sensing
Volume13
Number3
Pagese032509
Secondary MarkA2_GEOGRAFIA B1_GEOCIÊNCIAS B1_CIÊNCIAS_AGRÁRIAS_I B1_BIODIVERSIDADE B5_CIÊNCIAS_AMBIENTAIS
History (UTC)2019-08-07 11:05:46 :: simone -> administrator ::
2019-08-07 11:05:46 :: administrator -> simone :: 2019
2019-08-07 11:06:42 :: simone -> administrator :: 2019
2021-02-11 18:10:57 :: administrator -> simone :: 2019
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsCubeSat
state-dependent Riccati equation
Java
nonlinear
attitude
AbstractSTRaND and PhoneSat programs have attracted the attention of the aerospace community by applying, in CubeSats, commercial off-the-shelf smartphones based on Googles Android. In Android, the development commonly applies Java hence this language is a natural candidate for the attitude and orbit control subsystem (AOCS). Moreover, such AOCS can be designed with success by linear control theory; however, the linearized models are not able to represent all the effects of the nonlinear terms present in the dynamics. Therefore, nonlinear control techniques can yield better performance. An example is the Nano-Satellite Constellation for Environmental Data Collection, used as the reference in this work, a set of remote sensing CubeSats from the Brazilian National Institute for Space Research, in which the AOCS must stabilize the satellite in three-axes. We present the investigation of a state-dependent Riccati equation (SDRE) controller, a nonlinear controller, based on attitude errors given by quaternions. The investigation uses Java, accordingly, it can run on an Android operating system in a CubeSat, and it has low cost. Two controllers (linear and SDRE) were evaluated using a Monte Carlo perturbation model. The initial results show that the SDRE controller provides better performance.
AreaETES
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4. Conditions of access and use
data URLhttp://urlib.net/ibi/8JMKD3MGP3W34R/3TQ7C6P
zipped data URLhttp://urlib.net/zip/8JMKD3MGP3W34R/3TQ7C6P
Languageen
Target File032509_1.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policyallowpublisher allowfinaldraft
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 5
sid.inpe.br/mtc-m21/2012/07.13.14.54.10 4
DisseminationWEBSCI; PORTALCAPES; COMPENDEX; SCOPUS.
Host Collectionurlib.net/www/2017/11.22.19.04
6. Notes
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