Distributed control for a morphing wing with a macro fiber composite actuator
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F18%3A00328970" target="_blank" >RIV/68407700:21230/18:00328970 - isvavai.cz</a>
Výsledek na webu
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DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Distributed control for a morphing wing with a macro fiber composite actuator
Popis výsledku v původním jazyce
This work offers a new look at the morphing wing control, where the complex dynamical model is represented as a set of interconnected virtual agents and the distributed control paradigms are used. The background theme of this work is the most important of all aeroelastic phenomena causing unstable self-excited vibrations of aeroelastic structures like wings or ailerons. This instability called flutter occurs above the critical (flutter) speed where at least one of the modes is no longer damped. Aeroelasticity is relevant for the design of various structures including bridges, wind turbines, helicopter blades, and similar. This work considers specifically the flexible wing flutter.
Název v anglickém jazyce
Distributed control for a morphing wing with a macro fiber composite actuator
Popis výsledku anglicky
This work offers a new look at the morphing wing control, where the complex dynamical model is represented as a set of interconnected virtual agents and the distributed control paradigms are used. The background theme of this work is the most important of all aeroelastic phenomena causing unstable self-excited vibrations of aeroelastic structures like wings or ailerons. This instability called flutter occurs above the critical (flutter) speed where at least one of the modes is no longer damped. Aeroelasticity is relevant for the design of various structures including bridges, wind turbines, helicopter blades, and similar. This work considers specifically the flexible wing flutter.
Klasifikace
Druh
O - Ostatní výsledky
CEP obor
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OECD FORD obor
20205 - Automation and control systems
Návaznosti výsledku
Projekt
<a href="/cs/project/GA16-21961S" target="_blank" >GA16-21961S: Mechatronické struktury se silně distribuovanými aktuátory a senzory</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Ostatní
Rok uplatnění
2018
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů