4.7 Article

Event triggered control for fault tolerant control system with actuator failure and randomly occurring parameter uncertainty

Journal

APPLIED MATHEMATICS AND COMPUTATION
Volume 415, Issue -, Pages -

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.amc.2021.126714

Keywords

Event-triggered control; Fault tolerant control system; Actuator failure; Randomly occurring uncertainty; Passivity

Funding

  1. National Natural Science Foundation of China [11971444]

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This paper investigates the event-triggered control problem for fault-tolerant control system with actuator failure and randomly occurring parameter uncertainty. A hybrid event-triggered control scheme is adopted to greatly reduce network data transmission and save communication resources. The impact of actuator fault and random parameter uncertainty are studied under a unified framework, with conditions derived to guarantee the system's stochastic passivity. Simulation examples, including the F-404 aircraft engine system, are presented to illustrate the effectiveness of the proposed theoretical findings.
The paper investigates the event-triggered control problem for fault tolerant control system with actuator failure and randomly occurring parameter uncertainty. Firstly, the hybrid event-triggered control scheme is adopted for the fault tolerant control system subjected to actuator failure and randomly occurring parameter uncertainty in this paper, which could greatly decrease the amount of network data transmission and save communication resources. By utilizing the delay system method, the event-triggered fault tolerant control system is modeled as a delay system. Then, by constructing appropriate Lyapunov-Krasovskii functional, sufficient conditions are derived in form of linear matrix inequalities (LMIs) to guarantee the system is stochastically passive with prescribed passive performance gamma. The impact of the actuator fault and the random occurring parameter uncertainty are studied under the unified framework. Eventually, two simulation examples including F-404 aircraft engine system are presented to illustrate the effectiveness of the proposed theoretical findings. (C) 2021 Elsevier Inc. All rights reserved.

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