2019
DOI: 10.1016/j.ejcon.2019.04.008
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Robust passive adaptive fault tolerant control for stochastic wing flutter via delay control

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Cited by 17 publications
(10 citation statements)
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“…Generally, there are two major classes of FTC methods: active (AFTC) and passive (PFTC). In the PFTC approach, the FTC system cannot respond in real-time to all fault events since the controller's structure and its parameters are formerly set and trained to only tolerate a specific set of faults [4]. As a result, a PFTC approach cannot adjust its parameters to deal with the occurrence of faults, in real-time, that are not within the predefined set.…”
Section: Introductionmentioning
confidence: 99%
“…Generally, there are two major classes of FTC methods: active (AFTC) and passive (PFTC). In the PFTC approach, the FTC system cannot respond in real-time to all fault events since the controller's structure and its parameters are formerly set and trained to only tolerate a specific set of faults [4]. As a result, a PFTC approach cannot adjust its parameters to deal with the occurrence of faults, in real-time, that are not within the predefined set.…”
Section: Introductionmentioning
confidence: 99%
“…In the passive FTC category, the control system does not instantly respond to the online changes or occurrence of faults, while the controller is pre-designed, and its structure is fixed for both the faulty-free and the faulty cases. As a result, the control system will only exhibit certain robustness and tolerate a set of faults without any change in the structure of the controller [ 5 , 6 , 7 ]. Consequently, this type of controller is easy to implement.…”
Section: Introductionmentioning
confidence: 99%
“…Ming-Zhou and Guo-Ping 21 adopted the finite-time H adaptive fault-tolerant control technique to depress the vibration of the 2D wing airfoil. Recently, a robust passive adaptive fault control for a 2D airfoil model with control input delay was studied by Li et al 22 . In their study, a fault tolerant observer was designed to estimate the wing flutter states for control system.…”
Section: Introductionmentioning
confidence: 99%