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