Table 6 Comparison of Errors and Fit of the FAA Model Proposed in this paper with the FAA Models of15,16 under Varying Parameters.

From: A nonlinear multi-parameter model for predicting floor acceleration amplification across diverse structural systems

Parameter Model Name

MSE

MAE

\(R^2\)

\(R_\mu\)

Proposed model

0.05

0.18

0.84

Model C

0.09

0.25

0.73

Model S

0.14

0.30

0.58

\(T_1\)

Proposed model

0.04

0.15

0.85

Model C

0.05

0.19

0.79

Model S

0.09

0.24

0.63

z/h

Proposed model

0.05

0.18

0.84

Model C

0.09

0.24

0.73

Model S

0.14

0.30

0.58

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