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Chapter 5 Robust Performance Tailoring with Tuning - SSL - MIT

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FRF Magnitude: T z to OPD [µm/Nm]<br />

10 4<br />

10 2<br />

10 0<br />

10 −2<br />

10 −2<br />

Unconstrained<br />

<strong>with</strong> ACS Model<br />

10 −1<br />

10 0<br />

Frequency [Hz]<br />

Figure 2-3: Frequency response function of SCI: disturbance input Tz to performance,<br />

’-.’: <strong>with</strong>out ACS model, ’–’: <strong>with</strong> ACS.<br />

values are listed in Table 2.2. This method of modeling the ACS is simplistic, but will<br />

suffice for a model of this fidelity. The Fx and Fy transfer functions are not shown in<br />

Figure 2-3 since they are not affected by the rigid body modes.<br />

2.3.2 <strong>Performance</strong> Gradients<br />

A large number of optimization techniques, such as steepest descent, conjugate gradi-<br />

ent and Newtons method (see Appendix A), require the gradient of the performance<br />

<strong>with</strong> respect to the design variable, x. In the following discussion the gradients of the<br />

output variance are derived. For a more thorough presentation of these equations the<br />

reader is referred to the thesis by H. Gutierrez [50].<br />

To begin, notice that the performance metric is defined by Equation 2.14 <strong>with</strong> the<br />

constraint that Σq satisfies Equation 2.13. Therefore, the Lagrangian of the variance<br />

is written by augmenting the expression for the variance <strong>with</strong> a symmetric Lagrange<br />

multiplier matrix, Λi:<br />

� σ 2 zi<br />

�<br />

L = CiΣqC T i +Λi<br />

48<br />

10 1<br />

�<br />

AΣq +ΣqA T �<br />

T<br />

+ BB<br />

10 2<br />

(2.15)

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