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Adaptive Architectures for Control of Uncertain Dynamical Systems with Actuator Dynamics

Identifikátory výsledku

  • Kód výsledku v IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F18%3A00325171" target="_blank" >RIV/68407700:21230/18:00325171 - isvavai.cz</a>

  • Výsledek na webu

    <a href="http://dx.doi.org/10.2514/4.104794" target="_blank" >http://dx.doi.org/10.2514/4.104794</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.2514/4.104794" target="_blank" >10.2514/4.104794</a>

Alternativní jazyky

  • Jazyk výsledku

    angličtina

  • Název v původním jazyce

    Adaptive Architectures for Control of Uncertain Dynamical Systems with Actuator Dynamics

  • Popis výsledku v původním jazyce

    Stability properties of adaptive controllers can be seriously affected by the presence of actuator dynamics. Specifically, if the bandwidth of the actuator dynamics is sufficiently high, then a common practice is to neglect these dynamics in the design of adaptive controllers. However, if this is not the case and/or safety- critical applications of adaptive controllers are considered, then stability verification steps must be taken to show the allowable bandwidth range for actuators such that adaptive controllers lead to stable closed-loop system trajectories. Motivated from this standpoint, the purpose of this chapter is to present safe adaptive architectures for control of uncertain dynamical systems with actuator dynamics. We first present a linear matrix inequalities-based hedging framework, which modifies the ideal reference model trajectories to allow for correct adaptation that is not affected by the presence of actuator dynamics. Stability of the closed-loop dynamical system utilizing this framework is discussed using Lyapunov-based analysis tools. Next, we establish convergence properties of the modified reference model trajectories to the ideal reference model trajectories and present a generalization of the proposed linear matrix inequalities-based hedging framework to adaptive control. An algorithm is also presented to allow for less conservative computations of the minimum allowable actuator bandwidths as well as solving for cases in which there are multiple actuators. Finally, we illustrate the reported findings through an example on a linearized hypersonic aircraft model."

  • Název v anglickém jazyce

    Adaptive Architectures for Control of Uncertain Dynamical Systems with Actuator Dynamics

  • Popis výsledku anglicky

    Stability properties of adaptive controllers can be seriously affected by the presence of actuator dynamics. Specifically, if the bandwidth of the actuator dynamics is sufficiently high, then a common practice is to neglect these dynamics in the design of adaptive controllers. However, if this is not the case and/or safety- critical applications of adaptive controllers are considered, then stability verification steps must be taken to show the allowable bandwidth range for actuators such that adaptive controllers lead to stable closed-loop system trajectories. Motivated from this standpoint, the purpose of this chapter is to present safe adaptive architectures for control of uncertain dynamical systems with actuator dynamics. We first present a linear matrix inequalities-based hedging framework, which modifies the ideal reference model trajectories to allow for correct adaptation that is not affected by the presence of actuator dynamics. Stability of the closed-loop dynamical system utilizing this framework is discussed using Lyapunov-based analysis tools. Next, we establish convergence properties of the modified reference model trajectories to the ideal reference model trajectories and present a generalization of the proposed linear matrix inequalities-based hedging framework to adaptive control. An algorithm is also presented to allow for less conservative computations of the minimum allowable actuator bandwidths as well as solving for cases in which there are multiple actuators. Finally, we illustrate the reported findings through an example on a linearized hypersonic aircraft model."

Klasifikace

  • Druh

    C - Kapitola v odborné knize

  • CEP obor

  • OECD FORD obor

    20205 - Automation and control systems

Návaznosti výsledku

  • Projekt

  • Návaznosti

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Ostatní

  • Rok uplatnění

    2018

  • Kód důvěrnosti údajů

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

Údaje specifické pro druh výsledku

  • Název knihy nebo sborníku

    Advances in Computational Intelligence and Autonomy for Aerospace Systems

  • ISBN

    978-1-62410-478-7

  • Počet stran výsledku

    40

  • Strana od-do

    369-408

  • Počet stran knihy

    431

  • Název nakladatele

    AIAA

  • Místo vydání

    Reston, VA

  • Kód UT WoS kapitoly