TWIN ROTOR MIMO AERODYNAMICAL LABORATORY SYSTEM
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25530%2F10%3A39883360" target="_blank" >RIV/00216275:25530/10:39883360 - 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
TWIN ROTOR MIMO AERODYNAMICAL LABORATORY SYSTEM
Original language description
This paper presents the Twin Rotor MIMO Aerodynamical System (TRMAS). The Twin Rotor MIMO Aerodynamical System is a laboratory set-up designed for control experiments. In certain aspects its behaviour resembles that of a helicopter. From the control point of view it exemplifies a high order nonlinear system with significant cross-couplings. A mathematical model design of TRMS needs knowledge of aero dynamical physic laws. The TRMS consists of a beam pivoted on its base in such a way that it can rotate freely both in the horizontal and vertical planes. At both ends of the beam there are rotors (the main and tail ones) driven by DC motors. The state of the beam is described by four process variables: horizontal and vertical angles measured by encoders fitted at the pivot, and two corresponding angular velocities.
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
3
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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