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where R xxref<br />

is a vector consisting of R xi x ref<br />

. When the sensor node at location i has a<br />

time synchronization error of t xi<br />

relative to the reference node, the correlation function,<br />

<br />

can be written as<br />

R xi x ref<br />

R xi x ref<br />

= Ex i t – t xi<br />

+ x ref t = R xi x ref<br />

t – t xi<br />

<br />

(5.11)<br />

where E is the expectation operator. If t xi<br />

is positive, the correlation function for the<br />

interval (0, t xi<br />

) does not have the same characteristics as the succeeding signal. This<br />

portion of the cross correlation function will correspond to negative damping; therefore,<br />

the beginning portion of the signal needs to be removed. When t xi<br />

is unknown, a<br />

segment corresponding to the maximum possible time synchronization error, t xmax<br />

, is<br />

truncated from the correlation function.<br />

The correlation functions, each having independent time synchronization errors, do<br />

not satisfy the equation of motion, Eq. (5.10). The correlation functions after the<br />

truncation, R xi x ref<br />

' , however, can be decomposed into modal components as follows:<br />

R xi x ref<br />

' <br />

=<br />

'A<br />

'<br />

=<br />

2n<br />

=<br />

<br />

<br />

m<br />

– t x1<br />

–<br />

t x1<br />

2n –<br />

2n t x1<br />

<br />

–<br />

t x<br />

–<br />

t x<br />

2n2 –<br />

2n t x<br />

<br />

<br />

–<br />

<br />

t xm<br />

m<br />

–<br />

<br />

t xm<br />

2nm<br />

–<br />

2n<br />

t xm<br />

<br />

(5.12)<br />

= diag( <br />

<br />

<br />

<br />

2n<br />

<br />

)<br />

<br />

i<br />

= h i<br />

i<br />

+ j i<br />

– h i<br />

A = diag( a <br />

a <br />

a n<br />

)<br />

where ij<br />

is j-th element of i-th mode shape, h i<br />

and i<br />

are i-th modal damping ratio and<br />

modal natural frequency, respectively, and a i<br />

is a factor accounting for the relative<br />

contribution of the i-th mode in the correlation function matrix. Modal analysis techniques<br />

such as ERA can be used to identify these modal parameters. As Eq. (5.12) shows, the<br />

natural frequencies and damping ratios remain the same. The observed mode shapes '<br />

are, however, different from the original mode shapes; changes in mode shape amplitude<br />

are negligible due to small h i<br />

and t xi<br />

; however, phase shifts in the mode shapes can be<br />

substantial. Mode shape phases can indicate structural damage and are important modal<br />

characteristics from an SHM perspective. The requirements on time synchronization<br />

accuracy for modal analysis need to be assessed mainly from the viewpoint of the mode<br />

shape phase.<br />

76

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