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Keywords: Input‐output analysis
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Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2008) 80 (5): 545–548.
Published: 05 September 2008
... in Figure 5 when a failure occurs in “Sensor 4” at 7 s. In Figure 6 , the squared residual output can be shown when a fault occurs in “Sensor 4” at 7 s. © Emerald Group Publishing Limited 2008 Control technology Sensors Aircraft Failure (mechanical) Input‐output analysis...
