Structural Health Monitoring Using Smart Sensors - ideals ...
Structural Health Monitoring Using Smart Sensors - ideals ...
Structural Health Monitoring Using Smart Sensors - ideals ...
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Chapter 6<br />
ALGORITHMS<br />
In this chapter, algorithms for SHM to be implemented on smart sensors are<br />
discussed. The Distributed Computing Strategy (DCS) for SHM proposed by Gao (2005)<br />
has the potential to realize densely deployed networks of smart sensors for SHM, because<br />
of its local data sharing and processing. The algorithmic components of DCS for SHM,<br />
i.e., Natural Excitation Technique (NExT), Eigensystem Realization Algorithm (ERA),<br />
the Damage Locating Vector (DLV) method, and DCS, are briefly reviewed. Though most<br />
of the data processing is performed locally, the initialization phase of the strategy to<br />
estimate mode shape normalization constants involves more cumbersome processes; the<br />
initialization requires either input force measurement or output measurement before and<br />
after a known mass perturbation. Recent algorithmic developments of a stochastic DLV<br />
(SDLV) method by Bernal (2006) allows estimation of DLVs without input force<br />
measurement or mass perturbation. DCS is extended with this stochastic DLV method to<br />
allow for less demanding initialization.<br />
6.1 Natural Excitation Technique<br />
To understand the NExT (James et al., 1992, 1993) considered the equation of motion<br />
in Eq. (6.1) under the assumption of the stationary random process.<br />
Mx·· t<br />
+ Cx· t + Kx<br />
t = f<br />
t<br />
(6.1)<br />
where M , C, and K are the n x n mass, damping, and stiffness matrices, respectively;<br />
x<br />
t is a n x 1 displacement vector; f<br />
t is a m x 1 force vector; x· t and x·· t are the<br />
velocity and the acceleration vectors, respectively. By multiplying the displacement at the<br />
reference sensor and taking the expected value, Eq. (6.1) is transformed as follows:<br />
ME x·· t+x ref t + CEx· t+x ref t + KExt+x ref t+<br />
= Eft+x ref<br />
t <br />
(6.2)<br />
Because the input force and response at the reference sensor location are uncorrelated for<br />
, the right-hand side of Eq. (6.2) is zero. The expectation between the two signals is<br />
the correlation function. Therefore, by denoting Ext<br />
+ y<br />
t as the correlation<br />
function R xy<br />
, Eq. (6.2) is rewritten as<br />
MR x··xref<br />
+ CR x· xref<br />
+ KR xxref<br />
<br />
= <br />
<br />
(6.3)<br />
When At and Bt are weakly stationary processes, the following relation holds<br />
(Bendat & Piersol, 2000).<br />
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