1. Identity statement | |
Reference Type | Book Section |
Site | marte3.sid.inpe.br |
Holder Code | isadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S |
Identifier | 6qtX3pFwXQZ3r59YCT/H3K58 |
Repository | sid.inpe.br/iris@1905/2005/08.04.02.11 (restricted access) |
Last Update | 2019:01.18.16.44.01 (UTC) simone |
Metadata Repository | sid.inpe.br/iris@1905/2005/08.04.02.11.27 |
Metadata Last Update | 2021:02.03.17.56.01 (UTC) administrator |
Secondary Key | INPE-9542-PRE/5195 |
Label | 10470 |
Citation Key | Macau:2002:UsCoCh |
Title | Using control of chaos to control orbita motion in a hill problem |
Format | ISBN 85-17-00005-6 |
Year | 2002 |
Secondary Date | 20021213 |
Access Date | 2024, May 08 |
Secondary Type | PRE LN |
Number of Files | 1 |
Size | 3624 KiB |
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2. Context | |
Author | Macau, Elbert Einstein Neher |
Group | LIT-INPE-MCT-BR |
Editor | Winter, Othon Cabo Prado, Antonio Fernando Bertachini de Almeida. |
Book Title | Advances in space dynamics 2: applications in astronomy |
Publisher | INPE |
City | São José dos Campos |
Pages | 251-262 |
Series Title | Advances 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 |
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3. Content and structure | |
Is the master or a copy? | is the master |
Content Stage | completed |
Transferable | 1 |
Keywords | ENGENHARIA E TECNOLOGIA ESPACIAL chaos control orbits hill method |
Abstract | The 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. |
Area | ETES |
Arrangement | urlib.net > BDMCI > Fonds > Produção anterior à 2021 > COLIT > Using control of... |
doc Directory Content | access |
source Directory Content | there are no files |
agreement Directory Content | there are no files |
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4. Conditions of access and use | |
Target File | INPE-9542.pdf |
User Group | administrator |
Visibility | shown |
Read Permission | deny from all and allow from 150.163 |
Update Permission | not transferred |
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5. Allied materials | |
Next Higher Units | 8JMKD3MGPCW/444BQ9E |
Host Collection | sid.inpe.br/banon/2001/04.03.15.36 |
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6. Notes | |
Empty Fields | affiliation 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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