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1. Identity statement
Reference TypeJournal Article
Sitemtc-m21d.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34T/46ERJ6P
Repositorysid.inpe.br/mtc-m21d/2022/03.03.13.20
Metadata Repositorysid.inpe.br/mtc-m21d/2022/03.03.13.20.43
Metadata Last Update2023:01.03.16.46.01 (UTC) administrator
DOI10.2514/1.G006364
ISSN0731-5090
Citation KeySalazarPrad:2022:SuChMo
TitleSuppression of Chaotic Motion of Tethered Satellite Systems Using Tether Length Control
Year2022
Access Date2024, May 14
Type of Workjournal article
Secondary TypePRE PI
2. Context
Author1 Salazar, Francisco J. T.
2 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JGJA
ORCID1 0000-0002-3599-9745
2 0000-0002-7966-3231
Group1
2 DIMEC-CGCE-INPE-MCTI-GOV-BR
Affiliation1
2 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1
2 antonio.prado@inpe.br
JournalJournal of Guidance, Control and Dynamics
Volume45
Number3
Pages580-586
Secondary MarkA2_ENGENHARIAS_III
History (UTC)2022-03-03 13:20:44 :: simone -> administrator ::
2022-03-03 13:20:47 :: administrator -> simone :: 2022
2022-03-03 13:20:54 :: simone -> administrator :: 2022
2023-01-03 16:46:01 :: administrator -> simone :: 2022
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
AbstractA study introduces the out-of-plane motion in the local vertical and local horizontal positions, such that the initial states fall in the chaotic zone during the state-keeping phase. A tension force in the tether is applied to extend the tether until a maximum length and to suppress the chaotic behavior of the tethered satellite system (TSS). A linear approximation about the vertical position has been used, which leads to a linear tension control law (TCL) for tether deployment. The simulations show that the tension law performs well, and the chaotic motion can be guided to the stable vertical position. Terminal oscillations of the roll angle are encountered during deployment.
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