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1. Identity statement
Reference TypeBook Section
Sitemarte3.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier6qtX3pFwXQZ3r59YCT/H3K58
Repositorysid.inpe.br/iris@1905/2005/08.04.02.11   (restricted access)
Last Update2019:01.18.16.44.01 (UTC) simone
Metadata Repositorysid.inpe.br/iris@1905/2005/08.04.02.11.27
Metadata Last Update2021:02.03.17.56.01 (UTC) administrator
Secondary KeyINPE-9542-PRE/5195
Label10470
Citation KeyMacau:2002:UsCoCh
TitleUsing control of chaos to control orbita motion in a hill problem
FormatISBN 85-17-00005-6
Year2002
Secondary Date20021213
Access Date2024, May 08
Secondary TypePRE LN
Number of Files1
Size3624 KiB
2. Context
AuthorMacau, Elbert Einstein Neher
GroupLIT-INPE-MCT-BR
EditorWinter, Othon Cabo
Prado, Antonio Fernando Bertachini de Almeida.
Book TitleAdvances in space dynamics 2: applications in astronomy
PublisherINPE
CitySão José dos Campos
Pages251-262
Series TitleAdvances in space dynamics 2: applications in astronomy
History (UTC)2008-06-09 21:41:19 :: administrator -> jefferson ::
2012-08-02 17:55:11 :: jefferson -> administrator ::
2019-01-18 16:42:25 :: administrator -> simone :: 2002
2019-01-18 16:44:02 :: simone -> administrator :: 2002
2021-02-03 17:56:01 :: administrator -> :: 2002
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
chaos
control orbits
hill method
AbstractThe sensitive dependence on initial condition, which is the hallmark of chaos, has been exploited both theoretically and experimentally in the guidance of spacecraft. In general, chaos in a physical system implies accessibility to a wide range of system behaviors without requiring large perturbation. Thus, a chaotic trajectory can be used to accomplish interplanetary transfer operations expending very small amount of fuel. Besides the property of "sensitive dependence on initial condition, a chaotic invariant set has a dense set of unstable periodic orbits embedded in it. The well-known chaos control techniques use these orbits to stabilize chaotic trajectories. The purpose of this work is to show that the chaos control techniques can be used to efficiently keep a spacecraft around another body performing elaborate orbits. We consider a satellite and spacecraft moving initially in coplanar and circular orbits, with slightly different radii, around heavy central planet. The spacecraft, which is the inner body, has a slightly larger angular velocity than the satellite so that, after some time, they eventually go to a situation in which the distance between them becomes sufficiently small, so that they start to interact with one another. Considering this situation, we show that chaos control technique based on the OGY method can be used to keep the spacecraft in a desired orbit about a satellite. We also analyze the results and make considerations regarding a realistic scenario of space exploration.
AreaETES
Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > COLIT > Using control of...
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4. Conditions of access and use
Target FileINPE-9542.pdf
User Groupadministrator
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Next Higher Units8JMKD3MGPCW/444BQ9E
Host Collectionsid.inpe.br/banon/2001/04.03.15.36
6. Notes
Empty Fieldsaffiliation archivingpolicy archivist callnumber contenttype copyholder copyright creatorhistory descriptionlevel dissemination doi e-mailaddress edition electronicmailaddress isbn issn language lineage mark mirrorrepository nextedition notes numberofvolumes orcid parameterlist parentrepositories previousedition previouslowerunit progress project readergroup resumeid rightsholder schedulinginformation secondarymark serieseditor session shorttitle sponsor subject tertiarymark tertiarytype translator url versiontype volume


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