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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3KH6HGE
Repositorysid.inpe.br/mtc-m21b/2015/11.04.14.53
Last Update2015:11.04.14.53.48 (UTC) administrator
Metadata Repositorysid.inpe.br/mtc-m21b/2015/11.04.14.53.06
Metadata Last Update2021:02.11.21.57.01 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeySantosRocBogBenRem:2015:NoSoSp
TitleA novel solution for the spacecraft mixed actuators problem based on a multiobjective optimization method
Year2015
Access Date2024, May 16
Secondary TypePRE CI
Number of Files1
Size15702 KiB
2. Context
Author1 Santos, Willer Gomes dos
2 Rocco, Evandro Marconi
3 Boge, Toralf
4 Benninghoff, Heike
5 Rems, Florian
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
Group1 YYY-ETE-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 German Aerospace Center (DLR)
4 German Aerospace Center (DLR)
5 German Aerospace Center (DLR)
Author e-Mail Address1 willer.gomes@inpe.br
2 evandro.rocco@inpe.br
Conference NameInternational Symposium on Space Flight Dynamics, 25
Conference LocationMunich, Germany
Date19-23 Oct.
Book TitleProceedings
History (UTC)2015-11-04 14:53:06 :: simone -> administrator ::
2021-02-11 21:57:01 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typefinaldraft
KeywordsMixed Actuators Problem
Multiobjective Optimization
Final Approach Rendezvous
AbstractIn this paper, a novel solution for the mixed actuators problem is proposed. This approach uses a multiobjective optimization technique for commanding a group of actuators (thrusters, reaction wheels and magnetic torqrods) simultaneously optimizing a set of objective functions. The multiobjective problem is formulated using combinatorial combinations of the control signal for composing the decision space. The proposed model, called Actuator Multiobjective Command Method (AMCM), is included in a complete guidance, navigation and control loop applied to the final approach rendezvous scenario. Its performance, compared to different actuators configurations, has been evaluated in numerical simulations. In addition, AMCM has been integrated and tested in the hardware-in-the-loop rendezvous and docking simulator of the German Aerospace Center. Results have indicated effectiveness and robustness in both purely numerical and real-time simulations.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A novel solution...
Arrangement 2urlib.net > BDMCI > Fonds > Produção anterior à 2021 > YYY-PCI-CGETE > A novel solution...
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agreement Directory Content
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4. Conditions of access and use
data URLhttp://mtc-m21b.sid.inpe.br/ibi/8JMKD3MGP3W34P/3KH6HGE
zipped data URLhttp://mtc-m21b.sid.inpe.br/zip/8JMKD3MGP3W34P/3KH6HGE
Languageen
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/446AF4B
8JMKD3MGPCW/446B6T8
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.45.41 4
sid.inpe.br/bibdigital/2021/02.11.21.55 3
sid.inpe.br/mtc-m21b/2013/09.26.14.25.22 2
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsarchivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition editor format isbn issn label lineage mark nextedition notes numberofvolumes orcid organization pages parameterlist parentrepositories previousedition previouslowerunit progress project publisher publisheraddress rightsholder schedulinginformation secondarydate secondarymark serieseditor session shorttitle sponsor subject targetfile tertiarymark tertiarytype type url volume
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