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8/12/2019 Brincker_1
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Recent advances of Operational ModalRecent advances of Operational ModalAnalysis and applications in StructuralAnalysis and applications in Structural
Health MonitoringHealth Monitoring
Part one (OMA)Part one (OMA)Rune Brincker
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MotivationsMotivations
2
The mechanical engineer The civil engineer
SISO
MIMO
ODS
SISO
MIMO
ODS
OMAOMA
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Classical Modal AnalysisClassical Modal Analysis
3
Input
Output Signal
Time(Excitation) - Input
Working : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-200
-100
0
100
200
[s]
[N]
Time(Excitation) - Input
Working : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-200
-100
0
100
200
[s]
[N]
Time(Response) - Input
Working : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-80
-40
0
40
80
[s]
[m/s]
Time(Response) - Input
Working : Input : Input : FFT Analyzer
0 40m 80m 120m 160m 200m 240m
-80
-40
0
40
80
[s]
[m/s]
FFT
FFTInput Signal
Frequency Response H1(Response,Excitation) - Input (Magnitude)
Working : Input : Input : FFT Analyzer
0 400 800 1,2k 1,6k 2k 2,4k 2,8k 3,2k
10m
1
100
[Hz]
[(m/s)/N]
Frequency Response H1(Response,Excitation) - Input (Magnitude)
Working : Input : Input : FFT Analyzer
0 400 800 1,2k 1,6k 2k 2,4k 2,8k 3,2k
10m
1
100
[Hz]
[(m/s)/N]
Output Spectrum
Small structures
- easily tested
Artificial input provided no problemOutput
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Thinking of Civil EngineersThinking of Civil Engineers
4
Larger structures More slender structures Bigger loads
longer service New materials
Codes are getting bigger and bigger
Buildings are falling down
Even civil enginners NEEDS to know reallity
Cheaper and more accurate equipment
September 11, 1916.
Quebec Bridge (Canada)
*Images from http://www.engineeringcivil.com/theory/civil-engineering-disasters
December 15, 1967.
Silver Bridge (USA)
March 17, 1945.
Ludendor ff Bridge (Remagen, Germany)November 7, 2005.
(Almunecar, Spain)
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Idea of operatinal modal analysisIdea of operatinal modal analysis
5
MeasuredResponses
Stationary
Zero MeanGaussian
White Noise
Excitation Filter
(linear,
time-variant)
Structural System
(linear, time-
invariant)
Unknown excitation
forces
Combined System
Loading modes
Time-variant
Broad banded
Structural modes
Time-invariant
Narrow banded
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History on OMAHistory on OMA
6
Bendat & many others: Basic Frequency Domain
Andreas Felber PhD thesis
=
NNN
N
GG
GGGGG
L
OM
K
1
2221
11211
G
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Time domain techniqusTime domain techniqus
7
Sam Ibrahim and the Time Domain
Random Decrement Technique for Identification of Structures, J.
Spacecraft and Rockets, Vol. 14, No. 11, 1977
Sam Ibrahim and the Time Domain
Random Decrement Technique for Identification of Structures, J.
Spacecraft and Rockets, Vol. 14, No. 11, 1977
Henry Cole was looking for...
A simple and direct method for translating the time histori into a form
meaningful to the observer (1971)
Henry Cole was looking for...
A simple and direct method for translating the time histori into a form
meaningful to the observer (1971)
Vandiver, Brincker and Assmussen and the Random
Decrement (1982-1990)
Vandiver, Brincker and Assmussen and the Random
Decrement (1982-1990)
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0 2 4 6 8 10 12-5
0
5
10
15
20
25
30
SystemO
rder
Frequency(Hz)
20 40 60 80 100 120 140 160 180 2000
0.5
1
1.5
2
2.5
3
3.5Singular values of the system Hankel Matrix
index number of the singular values = 2*Model Order
IdentificationIdentification
8
PRCEH. Vold et al et al,1982
PRCEH. Vold et al et al,1982
ERAJuang and Pappa, 1985
ERAJuang and Pappa, 1985
MIMOMIMO
Could be used for OMA
Use RDD or correlation functions
Could be used for OMA
Use RDD or correlation functions
Developed on the basis of traditional
modal testing
Developed on the basis of traditionalmodal testing
But it did not (really) happenBut it did not (really) happen
Reasons: mode selection problem, no software...
Civil engineers were still sleeping...
Reasons: mode selection problem, no software...
Civil engineers were still sleeping...
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Begining of aplicationsBegining of aplications
9
First real test reported in
1993
Felber uses
the frequency domainsuccessfully
Felber uses
the frequency domainsuccessfully
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ApplicationsApplications
10
A.J.Felber & R.CantieniIntroduction of a new Ambient Vibration Testing System, EMPA,
1993-1996.
A.J.Felber & R.CantieniIntroduction of a new Ambient Vibration Testing System, EMPA,
1993-1996.
C.E.Ventura, A,J, Felber, S.F.StiemerDetermination of the dynamic characteristics of the colquiz Bridgebe full-scale testing, 1992.
C.E.Ventura, A,J, Felber, S.F.StiemerDetermination of the dynamic characteristics of the colquiz Bridge
be full-scale testing, 1992.
Tom Carne 1986Called it NExT= Correlation
functions+ Polyrefernce and
ERA
Tom Carne 1986Called it NExT= Correlation
functions+ Polyrefernce and
ERA
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ApplicationsApplications
11
Basic freq domain
SSI/ERA?
Updating
M.Hoeklie, O.E. HansteenMeasured and Predicted Dynamic Behavior
of the Gulfaks A Platform, 1988.
Basic frequency domain
Random decrement + Polyreference
J.C.Asmussen, R.Brincker, A.RytterAmbient modal testing of the vestvej bridge using random
decrement, 1998.
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Stochastic Subspace Identification: revival ofStochastic Subspace Identification: revival of
the time domainthe time domain
12
BUT: It sounds like black magic; Kalman gain matrix??? Projection of the Hankel matrix???
If you just need modal parameters forget about the Kalman gain matrix !
Bart de Moor and Overshees book in 1996 Data driven SSIBart de Moor and Overshees book in 1996 Data driven SSI
Very much like Random Decrement and time domain solved by SVD???
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Frequency domain decomposition: revival of theFrequency domain decomposition: revival of the
frequency domainfrequency domain
13
=
= UU
GGG
GGG
GGG
nnnnn
n
n
0
00
00
2
1
21
22221
11211
OMM
L
L
L
MOMM
L
L
G
( ) { } ( ) ( ) ( ) =
=
++ =
=
N
k
N
ik
jiji
kN
n
j
kn
i
nkjiji ekRGyykNyyEkR 0
2
,,
1
0
*
,
1
,
PSD Mag. Example SVD of PSD Matrix Decoupled Modes
Modal coordinate
auto spectral density( )1
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OverviewOverview
15
Reliable frequency domain techniques
Reliable time domain techniques
Using several data sets mode shapes
Many applications
Still problems: mode shape scaling... software, harmonics....
Reliable frequency domain techniques
Reliable time domain techniques
Using several data sets mode shapes
Many applications
Still problems: mode shape scaling... software, harmonics....
What do we have (around year 2000)?What do we have (around year 2000)?
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Scaling mode shapes (Mass change method)Scaling mode shapes (Mass change method)
16
Un-scaled mode shapes 1=T
=
1=MTScaled mode shapes
Scaling factor
Parloo et. al
MT
2=
Nomenclature :
Method:
Classical equation
KM =21
KM)(M =+
2
2
22
22
21 )( M 2M =
22221
MT22
=
Make a mass change
Subtraction
Solve forApproximation
Solve for
M
T2
2
22
21
=
Brincker et. al
1 2
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Approximation errorsApproximation errors
17
Simulation study
=
=
21
1..
.21
12
1
..
10
.01
km KM
20 DOF chainlike system
Mass change 0-20 % of DOF mass
Mathematical Model
22
2
2
1
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Approximation errorsApproximation errors
18
Errors should vanish for mass changes in increasing DOFsErrors should vanish for mass changes in increasing DOFs
Improved equationImproved equationM
T22
22
21
=Parloo equationParloo equation
MT
2=
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Error reductionError reduction
19
MM =
How to do it!
Do good ID and make large shift
Use improved equation
Do good ID and use many DOFs
Distribute mass change
How to do it!
Do good ID and make large shift
Use improved equation
Do good ID and use many DOFs
Distribute mass change
Error types
Random Error on frequency shift
Linearization error
Random Error on mode shape
Mode shape change error
Error types
Random Error on frequency shift
Linearization error
Random Error on mode shape
Mode shape change error
How can it be done (in an easy way) ?
Make a mass change and estimate the frequency shift
Easy: Shift masses around while using several data sets
How can it be done (in an easy way) ?
Make a mass change and estimate the frequency shift
Easy: Shift masses around while using several data sets
What is the accuracy ?
In a lausy test the typical uncertainty will be
around 10-20 %
In a well prepared test the typical uncertainty will
be around 2-5 %
What is the accuracy ?
In a lausy test the typical uncertainty will be
around 10-20 %
In a well prepared test the typical uncertainty will
be around 2-5 %
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Harmonic removalHarmonic removal
20
WithHarmoni
c
W
ithoutHarmonic
Harmonic Removal
Algori thm
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Harmonic removalHarmonic removal
21
( )( )2
2
2
22
1,|
==
x
exfy
( ) ( ){ }( ) ( ).sin.sin
sincos1|
1
1
Arc
ax
axfy
=
==
( ) ( )[ ] 3,|
4
4
=
xE
x
( ) 5.1. measmedian
Structural Modes:
Harmonics:
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Harmonic removalHarmonic removal
22
HarmonicRem
oval
Algorithm
HarmonicRemoval
Algorithm
Excluding Harmonic
Including Harmonic
Damping RatioNatural Frequency
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Known Harmonic RemovalKnown Harmonic Removal
23
* Notation adopted from P.Mohanty & D.J.Riexen
P.Mohanty & D.J.Riexen (2003-2005)
Modifications of Time domain Algorithms for Removing known Harmonic components
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Known Harmonic RemovalKnown Harmonic Removal
24
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[ ]is
f
f
ff
d
1
0f
1f 2f
f
Automated OMAAutomated OMA
25
Finding modes by FDDFinding modes by FDD
Modal coherenceModal coherence
Modal domainModal domain
Harmonics RemovalHarmonics Removal
FDD automatedFDD automated
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Modal CoherenceModal Coherence
26
)()()( 01101 fffd T
uu=
0)()( 101 =ffE T
uu NffVar T /1)()( 101 =uu
Discriminator function:
Low modal coherence: Noise
High modal coherence: Modal dominance
Random vectors:
Requirements:
. MAC level
. AveragingNumber
Requirements:
. MAC level
. AveragingNumber
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Modal DomainModal Domain
27
The modal domain is found as the Region around the peak whereThe modal domain is found as the Region around the peak where
)()()( 0112 fffd T
uu=
22 d
Discriminator function:
Mode property defined for all modes
Defines the frequency region dominated by
the mode
[ ]is
f
f
ff
d
1
0f
0f
1f 2f
f
Requirements:
MAC levelRequirements:
MAC level
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Example: Plate with HarmonicsExample: Plate with Harmonics
28
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Example: Heritage BuildingExample: Heritage Building
29
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Example: Z24 Highway BridgeExample: Z24 Highway Bridge
30
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ConclusionsConclusions
31
Valuable tools:Modal Coherence
Modal Domain
Harmonic discrimination
Dynamic headroom etc.
Important to note:It works..
Easier OMAApplications in health monitoring