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Matlab code for damping identification using energy ... - CFD4Aircraft

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Analytical integration of experimental data<br />

A single frequency sinusoidal function has been used to curve-fit the experimental measurements<br />

in order to use an analytical integration of accelerations to obtain velocities and<br />

displacements and to obtain an analytical expression of the integrals present in eq. (11).<br />

Considering a single test with an excitation at frequency ω i , vector g i (t) takethe<strong>for</strong>m<br />

⎧<br />

⎪⎨<br />

g i (t) =<br />

⎪⎩<br />

0<br />

0<br />

g i (t)<br />

0<br />

0<br />

0<br />

0<br />

0<br />

0<br />

0<br />

⎫<br />

⎪⎬<br />

⎪⎭<br />

(13)<br />

The input is assumed to be perfectly sinusoidal, so the measurement of g i (t) from the <strong>for</strong>ce<br />

transducer is fit to a harmonic function (figure 6) as<br />

g i (t) =r i sin(ω i t)+s i cos(ω i t) (14)<br />

by estimating the two coefficients r i and s i <strong>using</strong> least squares technique.<br />

8<br />

6<br />

Measured<br />

Sine-fit<br />

4<br />

Force (N)<br />

2<br />

0<br />

−2<br />

−4<br />

−6<br />

0 0.001 0.002 0.003 0.004 0.005 0.006 0.007 0.008 0.009 0.01<br />

Time (s)<br />

Figure 6: Typical measured and sine-fit <strong>for</strong>ce<br />

5

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