Distributed control for a morphing wing with a macro fiber composite actuator

Result code in 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>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Distributed control for a morphing wing with a macro fiber composite actuator
Original language description
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.
Czech name
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Czech description
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Project
<a href="/en/project/GA16-21961S" target="_blank" >GA16-21961S: Mechatronic structures with haevily distributed actuators and sensors</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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