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Shock and Vibration
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Shock and Vibration
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2020
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Article
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Fig 5
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Research Article
Recursive Method in Modal Parameter Identification of Aerospace Structures under Non-Gaussian Noise
Figure 5
EWRPLR-TARMA model order selection: (a) AR order, (b) MA order, and (c) forgetting factor.
(a)
(b)
(c)