Research Article

Model Parameter Estimation Method on Multichannel Structural Response from Turbulence Flutter Test

Table 3

System identification results of the physical test.

FSDDSSIProposed method
Frequency (Hz)Damping ratioFrequency (Hz)Damping ratioFrequency (Hz)Damping ratio

Horizontal tail signal10.3514.46110.5736.87111.3969.973
25.1864.94725.8364.45825.8206.594

Wing signal3.2287.6743.42410.4853.33717.92
6.5213.8616.8326.0836.7744.754
17.9734.48217.3566.83217.97213.881
32.2174.63432.6385.48932.6225.764