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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3MA6MP2
Repositorysid.inpe.br/mtc-m21b/2016/08.19.18.00   (restricted access)
Last Update2016:08.19.18.01.07 (UTC) simone
Metadata Repositorysid.inpe.br/mtc-m21b/2016/08.19.18.00.27
Metadata Last Update2021:02.11.20.56.38 (UTC) administrator
DOI10.1016/j.ymssp.2016.02.026
ISSN0888-3270
Citation KeyMainenti-LopesSouzSous:2016:CoStCo
TitleA comparative study between control strategies for a solar sailcraft in an Earth–Mars transfer
Year2016
MonthOct.
Access Date2024, May 19
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size913 KiB
2. Context
Author1 Mainenti-Lopes, I.
2 Souza, Luiz Carlos Gadelha de
3 Sousa, Fabiano Luis de
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
3 8JMKD3MGP5W/3C9JH3H
Group1
2 DMC-ETE-INPE-MCTI-GOV-BR
3 DSE-ETE-INPE-MCTI-GOV-BR
Affiliation1 Universidade de Brasília (UnB)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 rogimainemti@gmail.com
2 gadelha@dem.inpe.br
3 fabiano.sousa@inpe.br
JournalMechanical Systems and Signal Processing
Volume79
Pages289-296
Secondary MarkA1_ENGENHARIAS_III A1_ENGENHARIAS_I A2_ENGENHARIAS_IV B1_MATERIAIS B1_ENGENHARIAS_II B2_ASTRONOMIA_/_FÍSICA
History (UTC)2016-08-19 18:01:07 :: simone -> administrator :: 2016
2021-02-11 20:56:38 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsSolar sailcraft
Trajectory optimization
Evolutionary algorithm
Generalized extremal optimization
AbstractThe goal of this work was a comparative study of solar sail trajectory optimization using different control strategies. Solar sailcraft is propulsion system with great interest in space engineering, since it uses solar radiation to propulsion. So there is no need for propellant to be used, thus it can remains active throughout the entire transfer maneuver. This type of propulsion system opens the possibility to reduce the cost of exploration missions in the solar system. In its simplest configuration, a Flat Solar Sail (FSS) consists of a large and thin structure generally composed by a film fixed to flexible rods. The performance of these vehicles depends largely on the sails attitude relative to the Sun. Using a FSS as propulsion, an"Earth-Mars transfer optimization problem was tackled by the algorithms GEO(real1) and GEO(real2) (Generalized Extremal Optimization with real codification). Those algorithms are Evolutionary Algorithms (AE) based on the theory of Self-Organized Criticality. They were used to optimize the FSS attitude angle so it could reach Mars orbit in minimum time. It was considered that the FSS could perform up to ten attitude maneuvers during orbital transfer. Moreover, the time between maneuvers can be different. So, the algorithms had to optimize an objective function with 20 design variables. The results obtained in this work were compared with previously results that considered constant values of time between maneuvers.
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Arrangement 1urlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > A comparative study...
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4. Conditions of access and use
Languageen
Target Filemainenti_a comparative.pdf
User Groupsimone
Reader Groupadministrator
simone
Visibilityshown
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/446AF4B
8JMKD3MGPCW/446AUSL
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 4
sid.inpe.br/bibdigital/2021/02.11.20.54 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.51 3
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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