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Decentralized active damping control for aeroelastic morphing wing

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F23%3A00366657" target="_blank" >RIV/68407700:21220/23:00366657 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21230/23:00366657

  • Result on the web

    <a href="https://doi.org/10.1016/j.ast.2023.108415" target="_blank" >https://doi.org/10.1016/j.ast.2023.108415</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.ast.2023.108415" target="_blank" >10.1016/j.ast.2023.108415</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Decentralized active damping control for aeroelastic morphing wing

  • Original language description

    This paper introduces a novel decentralized control design procedure for an aeroelastic morphing wing. The control goal is active damping of this flexible system. The model is developed as a multi-agent system with inherent interconnections between the agents. The control system then takes advantage of the model structure and interconnections rather than relying on the entire system's model. This brings benefits, especially with a growing number of agents where the control design dimension remains low. Therefore, the proposed control design is especially suitable for morphing wings with a large number of actuation points. The result is presented in the Linear Matrix Inequalities (LMIs) form. A numerical example shows the application of the proposed algorithm.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    20205 - Automation and control systems

Result continuities

  • Project

    Result was created during the realization of more than one project. More information in the Projects tab.

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2023

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Name of the periodical

    Aerospace science and technology

  • ISSN

    1270-9638

  • e-ISSN

    1626-3219

  • Volume of the periodical

    139

  • Issue of the periodical within the volume

    August

  • Country of publishing house

    US - UNITED STATES

  • Number of pages

    10

  • Pages from-to

  • UT code for WoS article

    001013209800001

  • EID of the result in the Scopus database

    2-s2.0-85160721249