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Structural Health Monitoring Using Smart Sensors - ideals ...

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1<br />

Normalized accumulated stress<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

3 4 5 6 7 8 9 1011 7 8 9 10 111213 1415 1112 1314 151617 1819<br />

Element ID<br />

Figure 8.8. Normalized accumulated stress in sensor community 1, 2, and 3 (the SDLV<br />

method).<br />

by the three cluster head nodes. Element 8 is detected as an element with the normalized<br />

accumulated stress smaller than the threshold value, 0.3.<br />

The intermediate and final results of the two DLV methods such as singular values,<br />

DLVs, and the normalized accumulated stress are also calculated on a PC based on the<br />

centrally collected acceleration time histories. The results calculated on the Imote2 are the<br />

same as those on the PC with the same precision of the data type.<br />

The damage detection capability of the proposed SHM framework implemented on a<br />

network of Imote2s has been demonstrated in this section. Further investigation of the<br />

capabilities of the approach will be pursued in section 8.8 by replacing other elements of<br />

the truss.<br />

8.5 DCS logic<br />

Upon completing calculation of the normalized accumulated stresses, the three cluster<br />

heads exchange their damage detection results to perform the DCS logic given in Figure<br />

7.22. The log of the associated session recorded on the base station is presented in Figures<br />

8.9 and 8.10. These figures correspond to the damage detection results in Figures 8.7 and<br />

8.8, respectively. Because no inconsistency is reported, retake flags are set to zero as<br />

indicated by lines2, 9, and 16 in Figures 8.9 and 8.10. When no inconsistency is found, the<br />

results are reported to the base station, and the Imote2s prepare to enter a sleep mode.<br />

Though element 18 is identified as a damaged element by the mass perturbation DLV<br />

method, this false-positive is likely to be avoided if sensor community 4 also monitors this<br />

element because of the redundancy. When inconsistency is detected, the DCS algorithm is<br />

repeatedly applied. Figure 8.11 shows the report to the base station when inconsistency is<br />

observed. Sensor communities 3, 4, and 5 monitor the truss to detect damage at element<br />

21. Sensor communities 3 and 4 organized by cluster head nodes 73 and 135 find<br />

inconsistency. Sensor community 3 identifies element 16 as damaged, while sensor<br />

community 4 does not. After all three cluster heads finish reporting, only sensor<br />

communities 3 and 4 repeat acceleration measurement and data processing. The DCS<br />

143

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