Adaptive control design for the aeroelastic wing

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F21%3A00350824" target="_blank" >RIV/68407700:21220/21:00350824 - isvavai.cz</a>
Alternative codes found
RIV/68407700:21230/21:00350824
Result on the web
<a href="http://dx.doi.org/10.1109/PC52310.2021.9447451" target="_blank" >http://dx.doi.org/10.1109/PC52310.2021.9447451</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/PC52310.2021.9447451" target="_blank" >10.1109/PC52310.2021.9447451</a>

Result language
angličtina
Original language name
Adaptive control design for the aeroelastic wing
Original language description
The design of adaptive control for an aeroelastic wing using structured Hinfinity synthesis is presented in this paper. The algorithm uses a polynomial interpolation of controller parameters for a wide airspeed range. The structure of control law is fixed, with its parameters determined for a given airspeed range. We demonstrate the possibilities of such a controller for active flutter suppression on the linear parameter-varying (LPV) servoaeroelastic wing model with two ailerons.
Czech name
—
Czech description
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Project
<a href="/en/project/GA19-16772S" target="_blank" >GA19-16772S: Aerodynamic bodies with actively controlled morphing</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Proceedings of the 23rd International Conference on Process Control
ISBN
978-1-6654-0330-6
ISSN
—
e-ISSN
—
Number of pages
4
Pages from-to
225-228
Publisher name
IEEE
Place of publication
Piscataway
Event location
Štrbské Pleso
Event date
Jun 1, 2021
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000723653400038

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