Search Results - "Kure, Matej"

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  1. 1

    Stability optimization of time-delay systems with zero-location constraints applied to non-collocated vibration suppression by Saldanha, Adrian, Michiels, Wim, Kuře, Matěj, Bušek, Jaroslav, Vyhlídal, Tomáš

    Published in Mechanical systems and signal processing (15-02-2024)
    “…We present an active control method for achieving non-collocated vibration absorption, implemented on a lumped mass system. The task of suppressing vibrations…”
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    Journal Article
  2. 2

    Spectral Design and Experimental Validation of Noncollocated Vibration Suppression by a Delayed Resonator and Time-Delay Controller by Silm, Haik, Kure, Matej, Busek, Jaroslav, Michiels, Wim, Vyhlidal, Tomas

    “…A generally applicable spectral design to realize noncollocated vibration suppression performed primarily by a delayed resonator (DR) is presented. The…”
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    Journal Article
  3. 3

    Robust delayed resonator with acceleration feedback — design by double root assignment and experimental validation by Kuře, Matěj, Bušek, Jaroslav, Boussaada, Islam, Michiels, Wim, Niculescu, Silviu-Iulian, Vyhlídal, Tomáš

    Published in Journal of sound and vibration (28-04-2024)
    “…A combination of analytical and numerical time-delay system spectrum-shaping tools are applied to the design of the robust delayed resonator with an…”
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    Journal Article
  4. 4

    Algorithms for cable-suspended payload sway damping by vertical motion of the pivot base by Kuře, Matěj, Bušek, Jaroslav, Vyhlídal, Tomáš, Niculescu, Silviu-Iulian

    Published in Mechanical systems and signal processing (15-02-2021)
    “…•Payload swing damping by the pivot vertical motion is feasible by nonlinear control.•The problem is not controllable in the linear system sense.•Exponential…”
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    Journal Article
  5. 5

    Swing compensation of a payload suspended to a planar copter by Kure, Matej, Busek, Jaroslav, Vyhlidal, Tomas

    “…A switching strategy to compensate copter's sus- pended payload swing is presented. In order to prevent the payload swing during the maneuvers, the inverse…”
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    Conference Proceeding