Close

1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3KMHEKP
Repositorysid.inpe.br/mtc-m21b/2015/12.01.16.56   (restricted access)
Last Update2017:07.21.17.47.10 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2015/12.01.16.56.18
Metadata Last Update2021:02.11.18.12.31 (UTC) administrator
DOI10.2514/1.A33178
ISSN0022-4650
Citation KeySantosRocBogBenRem:2015:MuOpAp
TitleMulti-objective optimization applied to real-time command problem of spacecraft thrusters
Year2015
Access Date2024, Apr. 19
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size5165 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 (DLR)
4 German Aerospace Center (DLR)
5 German Aerospace Center (DLR)
Author e-Mail Address1 willer.gomes@inpe.br
2 evandro.rocco@inpe.br
JournalJournal of Spacecraft and Rockets
Volume52
Number5
Pages1407-1416
Secondary MarkA2_ENGENHARIAS_III B1_INTERDISCIPLINAR B1_ENGENHARIAS_IV
History (UTC)2015-12-01 16:56:18 :: simone -> administrator ::
2016-06-21 18:53:04 :: administrator -> simone :: 2015
2017-07-21 17:47:10 :: simone -> administrator :: 2015
2021-02-11 18:12:31 :: administrator -> simone :: 2015
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsCoupling problem
Force and torques
Guidance
navigation
and controls
Management functions
Reaction control system
Simulation framework
Single objective optimization
Spacecraft thrusters
AbstractA novel approach to solve the real-time command problem of spacecraft thrusters, called the thruster multiobjectivecommand method, is proposed in this paper. The reaction control system technology uses a set of thrusters in a special setup to simultaneously provide force and torque to the spacecraft. The thruster management function calculates all the candidate solutions that solve the thruster coupling problem. Then, a discrete multi-objective optimization method selects at every control cycle the best combination of thrusters and their firing time duration, which simultaneously optimizes a group of four objectives: the force error, the torque error, the propellant mass consumption, and the total number of pulses. The proposed method is included in a coupled translational and attitude control system applied to the final approach rendezvous scenario. Furthermore, all elements of the guidance, navigation, and control loop are accurately designed and implemented in a simulation framework. Results indicate effectiveness, robustness, and a better performance when compared to the usual single-objective optimization case.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Multi-objective optimization applied...
Arrangement 2urlib.net > Fonds > Produção anterior à 2021 > DIDMC > Multi-objective optimization applied...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Content
agreement.html 01/12/2015 14:56 1.0 KiB 
4. Conditions of access and use
Languageen
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
Archiving Policydenypublisher allowfinaldraft
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/bibdigital/2021/02.11.18.06 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.41 2
sid.inpe.br/bibdigital/2013/10.14.00.13 1
DisseminationWEBSCI; COMPENDEX; SCOPUS.
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
Empty Fieldsalternatejournal archivist callnumber copyholder copyright creatorhistory descriptionlevel e-mailaddress format isbn label lineage mark month nextedition notes orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey session shorttitle sponsor subject targetfile tertiarymark tertiarytype url
7. Description control
e-Mail (login)simone
update 


Close