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Structural load alleviation using distributed delay shaper: Application to flexible aircraft

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F19%3A00331829" target="_blank" >RIV/68407700:21230/19:00331829 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.1016/j.conengprac.2019.05.005" target="_blank" >https://doi.org/10.1016/j.conengprac.2019.05.005</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1016/j.conengprac.2019.05.005" target="_blank" >10.1016/j.conengprac.2019.05.005</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Structural load alleviation using distributed delay shaper: Application to flexible aircraft

  • Original language description

    Lightweight flexible aircraft suffers from unwanted oscillatory vibrations during aircraft manoeuvres. A recently developed distributed-delay signal (DZV) shaper is therefore proposed to be applied as a feedforward controller to alleviate the manoeuvre loads, as an alternative to traditional structural filters used routinely in this context. Structural filters are essentially linear low-pass filters with bandwidth below the significant flexible modes, applied to control signals generated either by the pilot’s direct input or by the flight control system. It has been showed that if instead a properly tuned signal shaper is used, better performance can be achieved: first, the target modes are significantly attenuated while the responsiveness of the aircraft is less compromised and secondly, the oscillatory nature of the vibrations are reduced. The high fidelity simulation results on a full scaled dynamic model of a highly flexible blended wing–body (BWB) aircraft show that in comparison to traditional structural filters, signal shapers significantly reduce the wing root loading (forces and moments) which provides potential structural benefits.

  • 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

    <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)

Others

  • Publication year

    2019

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Control Engineering Practice

  • ISSN

    0967-0661

  • e-ISSN

    1873-6939

  • Volume of the periodical

  • Issue of the periodical within the volume

    89

  • Country of publishing house

    GB - UNITED KINGDOM

  • Number of pages

    13

  • Pages from-to

    130-142

  • UT code for WoS article

    000477785800011

  • EID of the result in the Scopus database

    2-s2.0-85066394640