All

What are you looking for?

All
Projects
Results
Organizations

Quick search

  • Projects supported by TA ČR
  • Excellent projects
  • Projects with the highest public support
  • Current projects

Smart search

  • That is how I find a specific +word
  • That is how I leave the -word out of the results
  • “That is how I can find the whole phrase”

Controller design for highly maneuverable aircraft technology using structured singular value and direct search method

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F20%3A63526129" target="_blank" >RIV/70883521:28140/20:63526129 - isvavai.cz</a>

  • Result on the web

    <a href="https://ieeexplore.ieee.org/document/9214017" target="_blank" >https://ieeexplore.ieee.org/document/9214017</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1109/ICUAS48674.2020.9214017" target="_blank" >10.1109/ICUAS48674.2020.9214017</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Controller design for highly maneuverable aircraft technology using structured singular value and direct search method

  • Original language description

    The algebraic approach is applied to the HiMAT (Highly Maneuverable Aircraft Technology) control. The objective is to find a robust controller which guarantees robust stability and decoupled control of longitudinal model of a scaled remotely controlled vehicle version of the advanced fighter HiMAT. Control design is performed by decoupling the nominal multi-input multi-output system into two identical single-input single-output plants which are approximated by a 4th order transfer function. The algebraic approach is then used for pole placement design and the nominal closed-loop poles are tuned so that the peak of the μ-function is minimal. As an optimization tool, evolutionary algorithm Differential Migration is used in order to overcome the multimodality of the cost function yielding simple controller with decoupling for nominal plant which is compared with the D-K iteration through simulations of standard longitudinal manoeuvres documenting decoupled control obtained from algebraic approach for nominal plant as well as worst case perturbation. © 2020 IEEE.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • 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

    2020

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

  • ISBN

    978-1-72814-277-7

  • ISSN

  • e-ISSN

  • Number of pages

    5

  • Pages from-to

    529-533

  • Publisher name

    Institute of Electrical and Electronics Engineers Inc.

  • Place of publication

    Piscataway, New Jersey

  • Event location

    Athens

  • Event date

    Sep 1, 2020

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article

    000612041300069