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Online proceedings - EDA Publishing Association

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Check applicability<br />

Analytic / FE- modelling<br />

Check sensitivity<br />

Check orthogonality<br />

Development of test structures<br />

Characterization<br />

Fine grid of measurement points<br />

Selection of frequency modes for<br />

identification<br />

Parametet identification & validation<br />

Adaption of FE model<br />

Wafer-Test<br />

Fig. 2: Phases of the parameter identification<br />

The measurement time of a one point measurement is 2<br />

seconds. The measurement respectively software system is<br />

not yet optimized, the lower measurement time limit given<br />

by physics is about 200 milliseconds.<br />

Precondition for the identification is on one hand the<br />

measurement unit which delivers a FRF, and the simulation<br />

unit with a parameter matrix as result on the other hand. The<br />

automatic identification is done by a tool implemented in<br />

C++ with respect to a fast data processing. The<br />

identification tool can be structured into three submodules.<br />

The frequency values has to be extracted from the measured<br />

FRF which is done in one submodule, and the parameter<br />

matrix is approximated by usually polynomials in another<br />

submodule due to a fast and efficient data handling. Based<br />

on an user defined accuracy (default value 0.1%) the degree<br />

of the polynomial is selected by the program.<br />

Finally the optimization respectively identification is<br />

realized by the nonlinear least square method.<br />

Measurement<br />

system<br />

Frequency<br />

response<br />

Peak detection<br />

Identification tool<br />

Optimization<br />

FE-Simulation<br />

Polynomial<br />

approximation<br />

11-13 <br />

May 2011, Aix-en-Provence, France<br />

<br />

first step a conventional algorithm searches for local maxima<br />

considering the estimated signal-to-noise ratio (SNR). At the<br />

peaks found, starting values for a nonlinear least square fit to<br />

the Lorentzian function<br />

Parameter<br />

matrix<br />

i<br />

2<br />

, ih<br />

LfL<br />

, ip 2 2<br />

,<br />

)(<br />

+−<br />

, i hi<br />

)(<br />

f<br />

= (1)<br />

fff<br />

with the peak amplitude L p,i , the peak frequency f p,i and the<br />

half-width f h,i. of the ith peak are estimated. The iterative<br />

fitting procedure based on Levenberg-Marquardt algorithm<br />

eliminates wrongly preselected peaks and delivers the peak<br />

parameter including the quality factor.<br />

A. FE Modeling and Simulation<br />

The FE model which delivers the parameter matrices is<br />

implemented in Ansys. The ratio thickness to lateral<br />

dimension of the membrane leads to a modeling by twodimensional<br />

shell elements. The default mesh of the<br />

membrane perforated by several thousand holes will be<br />

irregular. To prevent such an inefficient irregular mesh<br />

substructures are generated. Square areas with a centered<br />

hole permit a regular meshing.<br />

Fig. 4: FE modell with prestructured membrane elements<br />

A prestressed modal analysis as well as a prestressed<br />

harmonic analysis is performed. The multitude of small<br />

structures causes a large number of finite elements<br />

respectively nodes. With regard to the measurement time the<br />

membrane symmetry is used by the calculation of a quarter<br />

model. Symmetric boundary conditions are applied to the<br />

static analysis. The modal analysis is executed with three<br />

load steps with different symmetry conditions at the x and y<br />

axes (symmetric/symmetric, asymmetric/symm. and<br />

asym./asym.) to deliver all modal frequencies .<br />

For the modeling of the squeeze film damping the<br />

corresponding element types of Ansys are used. The macro<br />

RMFLVEC.MAC which extracts the damping parameters<br />

from the modal frequencies is adapted to the quarter model<br />

with the multiple loadsteps.<br />

Sensor parameter<br />

Fig. 3: Structure of the parameter identification<br />

From the measured FRF, the peak frequency values are<br />

extracted automatically by a two level algorithm. Within a<br />

a) f 11 b) f 12<br />

Fig. 5: Simulated modal frequencies<br />

345

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