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Flexible aircraft lateral control law of low order

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F12%3A00187571" target="_blank" >RIV/68407700:21230/12:00187571 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Flexible aircraft lateral control law of low order

  • Original language description

    Overview of European collaborative project is presented in this paper and some results on lateral control law design for Blended Wing Body (BWB) type aircraft are given. Rigid body motions as well as flexible dynamic of the aircraft are considered. Recently developed Hinfinity optimization tools for fixed order robust controller are used to device lateral control augmentation system (CAS) with extremely low complexity.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

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

    2012

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Czech Aerospace

  • ISSN

    1211-877X

  • e-ISSN

  • Volume of the periodical

    2011

  • Issue of the periodical within the volume

    2

  • Country of publishing house

    CZ - CZECH REPUBLIC

  • Number of pages

    4

  • Pages from-to

    1-4

  • UT code for WoS article

  • EID of the result in the Scopus database