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smart technologies for safety engineering

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Dynamic Load Monitoring 113<br />

the second impact phase was 120–150 ms, while the duration of the whole phenomenon <strong>for</strong><br />

the analysed structure was 170–200 ms.<br />

4.1.6 Experimental Verification<br />

The impact identification approaches proposed in the previous subsections were verified experimentally<br />

with the described laboratory test stand. Each of the approaches was tested with<br />

a wide variety of 56 different impact scenarios admissible by the stand:<br />

seven masses spaced in the range 7.2–37.2 kg;<br />

eight drop heights equally spaced in the range 0.05–0.40 m, which corresponds to the impact<br />

velocities in the range of approximately 1–2.8 m/s.<br />

4.1.6.1 Solution Map Approach<br />

The objective was the maximum simplicity of the data acquisition set-up, i.e. to apply an<br />

algorithm able to operate on the basis of measurements from one sensor only. Moreover,<br />

an important issue was to use a sensor that was not directly fixed to the falling mass.<br />

It was decided to use the <strong>for</strong>ce sensor. Two impact parameters (mass m and velocity v<br />

of the falling body) had to be identified using the single <strong>for</strong>ce sensor. There<strong>for</strong>e, in order<br />

to construct the solution map, at least two characteristic quantities had to be extracted<br />

from only one measured <strong>for</strong>ce history. Figure 4.8 shows an example of <strong>for</strong>ce measurement<br />

Figure 4.8 Measured impact <strong>for</strong>ce evolution and parameters used to construct the solution map

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