2022
DOI: 10.1002/rnc.6431
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Dual‐terminal event‐triggered dynamic output feedback H∞ control for aero engine networked control systems with quantization

Abstract: This study deals with the problem of dual‐terminal event‐triggered dynamic output feedback (DOF) control for aero engine networked control systems (NCSs) subject to network‐induced delay, external disturbance, and quantization effects. First, we established a generalized mathematical model of the aero engine. Second, a dual‐terminal dynamic event‐triggered mechanism (DETM) was designed to reduce the utilization of the network bandwidth. In addition, a DOF controller with a compensation function was proposed to… Show more

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Cited by 7 publications
(3 citation statements)
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References 43 publications
(55 reference statements)
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“…When the system ( 13) is only subject to the event-triggered threshold condition (2), according to Corollary 1, we can obtain the controller design approach for the asymptotically stability of systematic system (26).…”
Section: Controller Co-design For Dual Event-triggered Networked Cont...mentioning
confidence: 99%
See 1 more Smart Citation
“…When the system ( 13) is only subject to the event-triggered threshold condition (2), according to Corollary 1, we can obtain the controller design approach for the asymptotically stability of systematic system (26).…”
Section: Controller Co-design For Dual Event-triggered Networked Cont...mentioning
confidence: 99%
“…In networked control systems, the channel resources from the controller-actuator (CA) are also constrained by bandwidth resources. At present, there are some research studies on introducing an ETM from the CA to raise the level of network resource utilization [26][27][28][29]. Li et al [30] modeled the closed-loop system as one that exhibits double event-triggered and network-induced delays and studied the dual event-triggered output feedback H ∞ control of NCSs with a networkinduced delay.…”
Section: Introductionmentioning
confidence: 99%
“…The inherently nonlinear nature of aero-engines presents a challenge when applying existing nonlinear control theories to this complex system. As a result, most accepted approaches rely on linear systems theory for aero-engine control theory [1][2][3]. However, this requires the nonlinear models to be transformed into linear forms that are more amenable for analysis and control design, which can be a daunting task.…”
Section: Introductionmentioning
confidence: 99%