Design and Analysis of Robust Fault Diagnosis Schemes for a Simulated Aircraft Model

<table>NLGA residuals for the 1st input sensor fault isolation with <svg height="10.6875" id="M533" style="vertical-align:-0.0pt" version="1.1" viewbox="0 0 7.9375 10.6875" width="7.9375" xmlns="http://www.w3.org/2000/svg">
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Journal of Control Science and Engineering

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Figure 2

Figure 2: Design and Analysis of Robust Fault Diagnosis Schemes for a Simulated Aircraft Model 