Research Article
Recursive Method in Modal Parameter Identification of Aerospace Structures under Non-Gaussian Noise
| | Initialization: | | | | | | Computation : | | | | | | | | | | | | | | | | | | | | | | | | Computation : | | | Downsizing: obtain by removing the first row and column of . | | | Compute according to the downsized matrix inversion formula. | | | | | | | | | | | | | | | | | | | | | | | | TARMA model parameter estimation: | | | |
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