2004
DOI: 10.1016/j.conengprac.2003.11.012
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Fault diagnosis for a turbine engine

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Cited by 34 publications
(16 citation statements)
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“…Turbomachinery performance deterioration analysis can be achieved by inducing deliberately some defects in the machine [7], or by building a model that simulates the conditions of mal function [8].…”
Section: Introductionmentioning
confidence: 99%
“…Turbomachinery performance deterioration analysis can be achieved by inducing deliberately some defects in the machine [7], or by building a model that simulates the conditions of mal function [8].…”
Section: Introductionmentioning
confidence: 99%
“…Fault sensitivity of fault diagnosis refers to the ability to correctly determine the existence of a fault and then isolate its type. The fault-sensitivity result of the above fault-diagnosis scheme can also be achieved using a similar approach (Diao and Passino, 2000b).…”
Section: Performance Evaluationmentioning
confidence: 99%
“…Note that the effects of the faults are usually large; hence, the above assumptions can often be satisfied in real applications. (Refer to Diao and Passino (2000a) for the proof.) Fault sensitivity of fault diagnosis refers to the ability to correctly determine the existence of a fault and then isolate its type.…”
Section: Performance Evaluationmentioning
confidence: 99%
“…Proof: Consider the Lyapunov function candidate (32) Using vector derivatives and following [20] and [32], the time derivative of (32) is (33) Note that and the th derivative of the output error is so that (34) and from (13), (26), (29), and (27), the equation shown at the bottom of the next page holds true. Also, from (15)- (18), (23), and (24), we have Substitute the aforementioned equation into (33) and assume that the ideal parameters are constant (which is achieved by having and in (17) and (18) represent approximation errors from the time-varying part of system dynamics) so that and and substitute (30) and (31) into (33) Notice that we did not consider a projection modification to the previous update laws.…”
Section: Indirect Adaptive Controlmentioning
confidence: 99%
“…The general form of the model can be described as shown in (49)-(54) at the bottom of the page, where WF36 is the system input (the combustor fuel flow) and XNL XNH represents the system states (the fan rotor speed [32] and [34] for more details on how we have developed the nonlinear engine model using Takagi-Sugeno fuzzy systems).…”
Section: Simulation Examples: Jet Engine Controlmentioning
confidence: 99%