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
—