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On the internal stability of non-linear dynamic inversion: application to flight control

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F67985556%3A_____%2F17%3A00476150" target="_blank" >RIV/67985556:_____/17:00476150 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21230/17:00311425

  • Result on the web

    <a href="http://dx.doi.org/10.1049/iet-cta.2016.1067" target="_blank" >http://dx.doi.org/10.1049/iet-cta.2016.1067</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1049/iet-cta.2016.1067" target="_blank" >10.1049/iet-cta.2016.1067</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    On the internal stability of non-linear dynamic inversion: application to flight control

  • Original language description

    Aircraft are highly non-linear systems, but flight control laws are traditionally designed from a set of linearised models. Due to the application of linear control laws on a non-linear system, the real performance ability of the aircraft is not fully utilised. In addition, in adverse situations like near stall, the aircraft develops significant non-linearities, and linear control laws do not perform well. This study therefore considers the design of a longitudinal flight controller for a fixed-wing aircraft using non-linear dynamic inversion technique or, in terms of control theory, partial exact feedback linearisation. A novel contribution of this study is the proposed combination of three different automatic flight controllers that provide complete 3-DOF longitudinal control. A detailed analysis of the internal dynamics for each controller is also presented. It has been shown that for each controller the internal dynamics are stable. This makes the controller suitable for various flight conditions. The aims of these flight controllers are threefold.

  • 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/GA17-04682S" target="_blank" >GA17-04682S: Control of walking robots using collocated virtual holonomic constraints</a><br>

  • Continuities

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

Others

  • Publication year

    2017

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    IET Control Theory and Applications

  • ISSN

    1751-8644

  • e-ISSN

  • Volume of the periodical

    11

  • Issue of the periodical within the volume

    12

  • Country of publishing house

    GB - UNITED KINGDOM

  • Number of pages

    13

  • Pages from-to

    1849-1861

  • UT code for WoS article

    000405681300001

  • EID of the result in the Scopus database

    2-s2.0-85024485443