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Force (N)<br />

600<br />

500<br />

400<br />

300<br />

200<br />

100<br />

Normal force<br />

<strong>The</strong>oretical<br />

Experimental<br />

total shear force (N)<br />

300<br />

200<br />

100<br />

0<br />

-100<br />

-200<br />

<strong>The</strong>oretical<br />

Experimental<br />

Total hysteresis loop<br />

Friction Force (N)<br />

200<br />

150<br />

100<br />

50<br />

0<br />

-50<br />

-100<br />

-150<br />

Damper hysteresis loop<br />

<strong>The</strong>oretical<br />

Experimental<br />

0<br />

0 10 20 30 40 50 60<br />

Time (s)<br />

-300<br />

-0.2 -0.1 0 0.1 0.2<br />

TMD Stroke (m)<br />

-200<br />

-0.2 -0.1 0 0.1 0.2<br />

TMD Stroke (m)<br />

(d) Normal force (e) Total hysteresis loop (f) Damper hysteresis loop<br />

Figure 7 Comparison of experimental and theoretical results due to El Centro earthquake (PGA=500gal,<br />

N 0 =130 N).<br />

Definition of performance indices<br />

<strong>The</strong> comparison results were quantified by performance evaluations of the SAF-TMD system in terms of the<br />

five performance indices (J 1 -J 5 ) in Table 2. <strong>The</strong> indices J 1 and J 3 in Table 2 represent the peak response ratios of<br />

the structural displacement x p (t) and structural acceleration of the SAF-TMD system, respectively. <strong>The</strong> indices<br />

J 2 and J 4 represent the root-mean-square (RMS) response ratios of x p (t) and & x p , a ( t)<br />

, respectively. Performance<br />

index J 5 represents the peak TMD stroke of the SAF-TMD. Notably, indices J 1 to J 4 were all divided by the<br />

corresponding response values of the uncontrolled system (primary structure only), which are represented by<br />

symbols with a top bar in Table 2. <strong>The</strong>refore, for indices J 1 to J 4 , a value less than one implies that the<br />

SAF-TMD system has a lower response than that of the uncontrolled system.<br />

Table 2 Definition of performance indices<br />

Response Peak structural displacement RMS structural displacement<br />

max( x<br />

p<br />

( t))<br />

w / TMD<br />

RMS(<br />

x<br />

p<br />

( t))<br />

w / TMD<br />

Index J1<br />

=<br />

J<br />

2<br />

=<br />

max( x ( t))<br />

RMS(<br />

x ( t))<br />

p<br />

w / o TMD<br />

p<br />

w / o TMD<br />

Response Peak structural acceleration RMS structural acceleration<br />

Index<br />

max( && x<br />

p,<br />

a<br />

( t))<br />

w / TMD<br />

RMS(<br />

&& x<br />

p,<br />

a<br />

( t))<br />

w / TMD<br />

J<br />

3<br />

=<br />

J<br />

4<br />

=<br />

max( && x<br />

p,<br />

a<br />

( t))<br />

w / o TMD<br />

RMS(<br />

&& x<br />

p,<br />

a<br />

( t))<br />

w / o TMD<br />

Stroke<br />

Peak TMD stroke<br />

Index J = max( v ( ))<br />

5 s<br />

t<br />

Comparison of SAF-TMD and uncontrolled system responses<br />

To demonstrate the control efficiency of the SAF-TMD, this subsection compares the experimental seismic<br />

responses of the SAF-TMD system to the simulated responses of its uncontrolled counterpart system (primary<br />

structure only). In the uncontrolled system, simulated responses were used instead of experimental ones for two<br />

reasons: (1) the uncontrolled system easily exceeds the allowable displacement of 0.25m, which limits<br />

comparison with earthquakes in which PGA is larger. (2) For comparison purposes, it would be very difficult for<br />

the shaking table to generate two exactly same ground accelerations for the SAF-TMD and uncontrolled systems.<br />

<strong>The</strong>refore, simulations of the uncontrolled system for comparison purposes used the same ground acceleration<br />

measured in the SAF-TMD test and the same system parametric values shown in Table 1.<br />

Table 3 shows the performance indices of the SAF-TMD system when data for the selected earthquake was<br />

applied. Table 3 shows that, although the SAF-TMD is less effective in reducing the peak response (J 1 and J 3 ) of<br />

the system, it reduces the RMS structural displacement by 12-18% (see J 2 ) and the RMS structural acceleration<br />

by 12-17% (see J 4 ), as compared to the RMS responses of the uncontrolled system.<br />

Table 3 Performance indices of the SAF-TMD<br />

Earthquake<br />

PGA Disp. index Acc. index<br />

(gal) J 1 J 2 J 3 J 4<br />

300 0.98 0.88 1.03 0.88<br />

El Centro 400 0.94 0.84 0.99 0.85<br />

500 0.91 0.82 0.90 0.83<br />

-413-

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