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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m16.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Repositorysid.inpe.br/marciana/2004/07.20.16.07
Last Update2004:09.21.03.00.00 (UTC) administrator
Metadata Repositorysid.inpe.br/marciana/2004/07.20.16.07.15
Metadata Last Update2021:02.11.18.15.15 (UTC) administrator
Secondary KeyINPE-10979-PRE/6435
Citation KeyTrigoloSouzKuga:2004:FlSpSy
TitleFlexible space system states and parameters estimation
FormatOn-line
Year2004
Access Date2024, May 20
Secondary TypePRE CI
Number of Files1
Size279 KiB
2. Context
Author1 Trigolo, Adriana
2 Souza, Luiz Carlos Gadelha de
3 Kuga, Helio Koiti.
Resume Identifier1
2 8JMKD3MGP5W/3C9JHN3
Group1 DMC-INPE-MCT-BR
2 DMC-INPE-MCT-BR
3 DMC-INPE-MCT-BR
Conference NameSpace Flight Mechanics Meeting, 14
Conference LocationMaui, Hawai.
Date2004
PublisherAIAA
Book TitleProceedings
History (UTC)2006-11-09 18:43:49 :: administrator -> marciana ::
2007-03-20 13:35:50 :: marciana -> administrator ::
2021-02-11 18:15:15 :: administrator -> marciana :: 2004
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
KeywordsENGENHARIA E TECNOLOGIA ESPACIAL
Kalman Filter
flexible Euler- Bernoulli
mathematical model
AbstractNowadays an increasing number of space missions are using satellites with a rigid hub and long and/or wide flexible appendices, such as solar panels, communication antennas, telescopic structures, and robotics flexible arms. The increasing need for better pointing accuracy of antennas connected to the rigid part of the spacecraft leads to a requirement for more efficient controllers, where more accurate identification process play an important rule into the closed loop system. To meet the requirements for pointing accuracy, flexible parameters as elastic displacement, which are of great importance for control tasks should be continuously identified in the space environment. This paper presents investigation results of elastic displacement identification using the Kalman Filter methodology. A flexible Euler- Bernoulli beam, connected to a rigid core with torques as input and angles and angular velocities as outputs is used as simple mathematical model of a rigidflexible satellite to apply the Kalman filter identification algorithm proposed. The Kalman filter is tested under several conditions considering cold start with coarse initial knowledge and varied measurement noise levels. At the end comments are drawn about the robustness of the proposed procedure and feasibility of implementation within the control system loop.
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Arrangementurlib.net > BDMCI > Fonds > Produção anterior à 2021 > DIDMC > Flexible space system...
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data URLhttp://urlib.net/ibi/sid.inpe.br/marciana/2004/07.20.16.07
zipped data URLhttp://urlib.net/zip/sid.inpe.br/marciana/2004/07.20.16.07
Languageen
Target Fileflexible space system.pdf
User Groupadministrator
marciana
Visibilityshown
Copy HolderSID/SCD
Read Permissionallow from all
5. Allied materials
Next Higher Units8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/mtc-m21/2012/07.13.14.54.10 1
Host Collectionsid.inpe.br/banon/2003/08.15.17.40
6. Notes
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