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533<br />

cation corresponds to a node of one of the modes, that mode will not be observed. This<br />

method allows the cross spectral density (CSD) functions to be averaged over a number of<br />

samples to increase the accuracy in the CSDs. Windowing should be used to minimize the<br />

effects of leakage.<br />

Identification of Modal Parameters<br />

Once the time domain free response data is obtained, there are numerous techniques available<br />

for identifying the modal parameters Here the ERA (Juang and Pappa, 1985) is<br />

adopted because it is quite effective for identification of lightly damped structures and is<br />

applicable to multi-input/multi-output systems. In the ERA, the Hankel matrix is formed<br />

y(k)<br />

(5)<br />

where y(k) is the response vector at the £th time step. <strong>The</strong> parameters s and r correspond<br />

to the number of columns and rows (of response vectors) in the matrix. This matrix is<br />

evaluated for H(0) and a singular value decomposition is performed,<br />

H(0) = PDQ 7 (6)<br />

Relatively small singular values along the diagonal of D correspond to computational<br />

modes and the associated rows and columns are eliminated to form the condensed D^v,<br />

P jV , and Q N matrices. <strong>The</strong> state matrix for the resulting discrete time system and the associated<br />

matrix in the output equation are found using is found using<br />

_! _1 _!<br />

A = D^ 2P/H(l)QtfDtf 2 C - K T P N D N<br />

2<br />

where E r = [I 0. .0]. Because this is a discrete time system, it is then transformed to<br />

the corresponding continuous time system. <strong>The</strong> natural frequencies are found by determining<br />

the eigenvalues of the continuous time matrix A, and C is used to transform the computed<br />

eigenvectors of the state matrix corresponding to the non-physical states in the<br />

identified model, to the values of the mode shapes at the floors of the structure. <strong>The</strong> ERA<br />

method was implemented in MATLAB (1997).<br />

NUMERICAL RESULTS<br />

<strong>The</strong> approach described in the previous section was implemented to identify the modal parameters<br />

of the structure from simulated acceleration records. Uncorrelated stationary<br />

broadband forces were used as the excitation in the lateral, longitudinal and transverse directions.<br />

<strong>The</strong> excitations were applied along the deck of the bridge. Thirty minute acceleration<br />

record with a sampling rate of 12.5 Hz was used for the identification procedure.<br />

Three different sensor configurations were considered to study the capabilities of the<br />

methods when the number of sensors is varied. Figure 3 shows the identification models<br />

used and the location of the sensors on the bridge for each case. Three sensors in each tower<br />

measure accelerations in the transverse and longitudinal directions. All deck sensors<br />

measure acceleration in the transverse and vertical directions. Case 1 uses a total of 128<br />

(7)

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