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MODAL ANALYSIS - the Dept. of Mechanical Engineering at - Vrije ...

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2.2.2 Observability and Controllability <strong>of</strong> Modes<br />

Assuming, for example, th<strong>at</strong> one force is applied in DOF 1 while <strong>the</strong> displacement is observed in<br />

DOF 2. In th<strong>at</strong> case, <strong>the</strong> multiple-input-multiple-output (MIMO) transfer function m<strong>at</strong>rix simplifies<br />

to <strong>the</strong> following single-input-single-output (SISO) transfer function<br />

H<br />

2,<br />

1<br />

( s)<br />

= m N<br />

ψ<br />

( 2)<br />

⋅ψ<br />

( 1)<br />

ψ<br />

( 2)<br />

⋅ψ<br />

( 1)<br />

∗ ∗<br />

m m<br />

m m<br />

∑ +<br />

∗<br />

m= 1 s − λm<br />

s − λm<br />

If ψ n ( 1)<br />

≠ 0 <strong>the</strong>n mode n will only be “observed” in DOF 2 if ψ n ( 2)<br />

≠ 0 . If ψ n ( 1)<br />

= 0 <strong>the</strong>n it is<br />

clear th<strong>at</strong> <strong>the</strong> terms corresponding to mode n will not appear in <strong>the</strong> sum, i.e. mode n cannot be<br />

excited (or “controlled”) by applying a force in DOF 1. The DOFs where a mode shape vector<br />

equals zero are called nodal points or nodes. In practice, this means th<strong>at</strong> <strong>the</strong> force actu<strong>at</strong>or should<br />

not be positioned in a nodal point <strong>of</strong> <strong>the</strong> modes <strong>of</strong> interest. To reduce <strong>the</strong> risk <strong>of</strong> missing modes, <strong>the</strong><br />

number <strong>of</strong> excit<strong>at</strong>ion points can be increased. The same is true for <strong>the</strong> response measurements. The<br />

number <strong>of</strong> inputs (excit<strong>at</strong>ion points) is typically in <strong>the</strong> order <strong>of</strong> 1 to 10, while <strong>the</strong> number <strong>of</strong> outputs<br />

(response measurements) can reach more than 1000 points when using optical measurement<br />

equipment such as for instance a scanning laser Doppler vibrometer.<br />

3. Frequency-Domain Identific<strong>at</strong>ion <strong>of</strong> Modes<br />

Typical for modal analysis is <strong>the</strong> very large number <strong>of</strong> outputs. This huge amount <strong>of</strong> d<strong>at</strong>a requires<br />

dedic<strong>at</strong>ed algorithms th<strong>at</strong> balance between accuracy and memory/computing needs. In Section 3.1<br />

such a ‘dedic<strong>at</strong>ed’ frequency-domain least-squares estim<strong>at</strong>or will be presented. Based on <strong>the</strong>se<br />

results, it is possible to implement more sophistic<strong>at</strong>ed identific<strong>at</strong>ion methods (see 6.43.8.2<br />

Estim<strong>at</strong>ion with Known Noise Model and 6.43.8.4 Estim<strong>at</strong>ion with Unknown Noise Model) such as<br />

for instance <strong>the</strong> frequency-domain Maximum Likelihood (ML) estim<strong>at</strong>or (Section 3.2).<br />

3.1 Least Squares Estim<strong>at</strong>ion<br />

3.1.1 Common-Denomin<strong>at</strong>or Model<br />

The rel<strong>at</strong>ionship between output o ( o = 1, �,<br />

N o ) and input i ( i = 1, �,<br />

N i ) is modeled in <strong>the</strong><br />

frequency domain by means <strong>of</strong> a common-denomin<strong>at</strong>or transfer function<br />

ˆ N k ( ω)<br />

H k ( ω)<br />

= (20)<br />

d(<br />

ω)<br />

for k = 1, �,<br />

N o N i (where k = ( o −1)<br />

N i + i ) and with<br />

k<br />

n<br />

∑<br />

j=<br />

0<br />

N ( ω ) = Ω ( ω)<br />

B<br />

(21)<br />

j<br />

kj<br />

<strong>the</strong> numer<strong>at</strong>or polynomial between output o and input i and<br />

n<br />

∑<br />

j=<br />

0<br />

d(<br />

ω ) = Ω ( ω)<br />

A<br />

(22)<br />

j<br />

j<br />

<strong>the</strong> common-denomin<strong>at</strong>or polynomial. The real-valued coefficients j A and B kj are <strong>the</strong> parameters<br />

to be estim<strong>at</strong>ed. Several choices are possible for <strong>the</strong> polynomial basis functions Ω j (ω)<br />

. For a<br />

discrete-time domain model, <strong>the</strong> functions Ω j (ω)<br />

are usually given by Ω j ( ω ) = exp( −iωTs<br />

⋅ j)<br />

j<br />

(with T s <strong>the</strong> sampling period) while for a continuous-time domain model Ω ( ω ) = ( iω)<br />

. The bad<br />

j<br />

(19)

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