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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3MQ9H8L
Repositorysid.inpe.br/mtc-m21b/2016/11.14.12.12   (restricted access)
Last Update2016:11.14.12.12.13 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2016/11.14.12.12.13
Metadata Last Update2021:02.11.18.12.36 (UTC) administrator
DOI10.1007/s40295-016-0094-0
ISSN0021-9142
Citation KeySantosRocBogBenRem:2016:HaReTe
TitleHardware-in-the-loop rendezvous tests of a novel actuators command concept
Year2016
MonthDec.
Access Date2024, May 15
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size2132 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 CMC-ETES-SPG-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
4 German Aerospace Center
5 German Aerospace Center
Author e-Mail Address1 willer.gomes@inpe.br
2 evandro.rocco@inpe.br
3 toralf.boge@dlr.de
4 heike.benninghoff@dlr.de
5 florian.rems@dlr.de
JournalJournal of the Astronautical Sciences
Volume63
Number4
Pages287-307
Secondary MarkB1_ENGENHARIAS_III B5_ASTRONOMIA_/_FÍSICA
History (UTC)2016-11-14 12:12:13 :: simone -> administrator ::
2016-11-14 12:14:52 :: administrator -> simone :: 2016
2016-11-14 12:15:04 :: simone -> administrator :: 2016
2021-02-11 18:12:36 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsHardware-in-the-loop simulation
Spacecraft control system
Multiobjective optimization
On-orbit servicing mission
AbstractIntegration, test and validation results, in a real-time environment, of a novel concept for spacecraft control are presented in this paper. The proposed method commands simultaneously a group of actuators optimizing a given set of objective functions based on a multiobjective optimization technique. Since close proximity maneuvers play an important role in orbital servicing missions, the entire GNC system has been integrated and tested at a hardware-in-the-loop (HIL) rendezvous and docking simulator known as European Proximity Operations Simulator (EPOS). During the test campaign at EPOS facility, a visual camera has been used to provide the necessary measurements for calculating the relative position with respect to the target satellite during closed-loop simulations. In addition, two different configurations of spacecraft control have been considered in this paper: a thruster reaction control system and a mixed actuators mode which includes thrusters, reaction wheels, and magnetic torqrods. At EPOS, results of HIL closed-loop tests have demonstrated that a safe and stable rendezvous approach can be achieved with the proposed GNC loop.
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4. Conditions of access and use
Languageen
Target FileSantos_hardware.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher denyfinaldraft
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.45.41 5
sid.inpe.br/bibdigital/2021/02.11.18.06 2
sid.inpe.br/bibdigital/2013/10.14.00.13 1
DisseminationWEBSCI
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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