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Chapter 5 Robust Performance Tailoring with Tuning - SSL - MIT

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energy is distributed almost evenly among the first (ACS), third and eleventh (second<br />

axial) modes. The ACS mode and second axial mode contribute a small percentage<br />

to the output in the nominal design, but account for 38% and 26% of the energy,<br />

respectively, in the PT design. Comparing the natural frequencies, it is found that<br />

the PT design frequencies are at least a factor of two lower than those of the nominal<br />

design. The lower frequencies make sense considering the fact that the cross-sectional<br />

areas of the beam have decreased greatly from the nominal system (0.10 m) to the<br />

PT design (0.03 m). The cross-section diameters map directly to area and inertia<br />

(Equations 2.31 and 2.30) which in turn map to the stiffness matrix (Equation 2.2).<br />

Lowering the cross-sectional diameters lowers the global stiffness matrix of the system<br />

and, in turn, the natural frequencies.<br />

The final step in understanding the differences between the two systems is to ex-<br />

amine the mode shapes of the critical modes, plotted in Figure 2-8. The ACS mode<br />

changes between the two systems (Figure 2-8(a)) partly due to the change in inertia,<br />

which in turn effects the modal frequency. The shape of this mode (Figure 2-8(a))<br />

is similar in the nominal and PT design but its frequency is much lower in the tai-<br />

lored case (PT). There is a large difference in percent energy contribution from this<br />

mode between the two systems (from 14% to 38.5%), but the absolute RMS values<br />

accumulated in the motion are of similar magnitude (59 and 39µm).<br />

The major improvement in performance is due to the tailoring of the second<br />

bending mode (Figure 2-8(b)). Notice that in the nominal design the two outer nodal<br />

points, or points of zero deflection, are located slightly away from the endpoints of<br />

the array towards the center. However, in the PT design, these nodal points are right<br />

at the ends of the array, where the collectors are located. Since the collector motions<br />

feature prominently in the OPD equation (Equation 2.9), tailoring the mode shape<br />

such that the nodal points are located at the collectors significantly reduces the OPD<br />

output in this mode, and, as a result, the total RMS OPD.<br />

The second and fourth modes (Figures 2-8(c) and 2-8(d)) are account for zero<br />

energy in the nominal case, but a finite (although small) amount of energy in the PT<br />

design. In the nominal design the system is perfectly symmetric so these modes are<br />

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