2019 Chinese Control Conference (CCC) 2019
DOI: 10.23919/chicc.2019.8866614
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Adaptive Observer based Fault Tolerant Control for Aircraft Engine with Sensors and Actuators Faults

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Cited by 11 publications
(8 citation statements)
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“…Motivated by the growing need for safety and reliability, fault-tolerant control (FTC) is increasingly becoming an interesting approach in the past two decades, since it allows to reduce the faults effect and minimize human and material damage. Various applications of FTC are studied in the literature such as aircraft (Li et al, 2020; Xiao et al, 2019), wind turbine (Azizi et al, 2019; Wang et al, 2017) and spacecraft (Tao et al, 2019; Yi et al, 2019). The interested reader can refer, for instance, to Zhang and Jiang (2008) and Amin and Hasan (2019).…”
Section: Introductionmentioning
confidence: 99%
“…Motivated by the growing need for safety and reliability, fault-tolerant control (FTC) is increasingly becoming an interesting approach in the past two decades, since it allows to reduce the faults effect and minimize human and material damage. Various applications of FTC are studied in the literature such as aircraft (Li et al, 2020; Xiao et al, 2019), wind turbine (Azizi et al, 2019; Wang et al, 2017) and spacecraft (Tao et al, 2019; Yi et al, 2019). The interested reader can refer, for instance, to Zhang and Jiang (2008) and Amin and Hasan (2019).…”
Section: Introductionmentioning
confidence: 99%
“…Deriving (7) gives ṡ = ẋ + σx (9) Considering the nominal model of aircraft engine (4) and substituting (4a) into (9) yields ṡ = Ax + Bu + σx (10) Compare (10) with (8), it gives…”
Section: Sliding Mode Fault-tolerant Controller Designmentioning
confidence: 99%
“…In order to meet the performance optimization requirements in aircraft engines, Reference [9] presented a non-linear model predictive control method based on elastic back propagation (BP) neural network with hybrid grey wolf optimizer (GWO). On the basis of adaptive observer, Reference [10] proposed a faulttolerant control (FTC) method for aircraft engines with sensor faults and actuator faults. Reference [11] used the method of decoupling start control for aircraft wound-rotor synchronous starter-generator and achieved good results.…”
Section: Introductionmentioning
confidence: 99%
“…Zhang et al [10] studied the problem of fault estimation and designed adaptive observer. Xiao et al [11] studied the fault tolerant control for aircraft engine with sensors faults. However, they work for a single system.…”
Section: Introductionmentioning
confidence: 99%