ADAPTIVE CONTROL OF TWIN ROTOR MIMO SYSTEM
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25530%2F10%3A39883362" target="_blank" >RIV/00216275:25530/10:39883362 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
ADAPTIVE CONTROL OF TWIN ROTOR MIMO SYSTEM
Original language description
The laboratory helicopter simulator is a nonlinear two inputs - two outputs system with significant cross-coupling. Controlled variables are position angles (elevation and azimuth), manipulated variables are motor voltages. Self-tuning adaptive controller was designed and tested on the real system. On-line identification of linear model parameters was the first part of self-tuning algorithm and the controller design by internal model control (IMC) method was the second one. The adaptive control algorithm was used for tracking of the reference values of position angles.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BC - Theory and management systems
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Summaries volume 9th International Conference Process Control 2010
ISBN
978-80-7399-951-3
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
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Publisher name
Tribun EU
Place of publication
Brno
Event location
Kouty nad Desnou
Event date
Jun 7, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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