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Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Cincinnati, Ohio 45221-0072 USAWWW.SDRL.UC.EDU
(513) 556-2720
Copyr ight © 2001
SHAKER EXCITATION TUTORIAL
Considerations and Problems
Young Engineer’s Program - IMAC 2001
Excitation Tutor ial -1- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Typical Shaker Excitation Test Setup Schematic
Excitation Tutor ial -2- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Test Set-up for Shaker Excitation
• Physical Connections, Alignment
• Instrumentation
• Single Vs. Multiple Shakers
• Excitation Signal Type
• Digital Signal Processing
• Data Quality
• Post-Test Considerations
• Modal Parameter Estimation
Excitation Tutor ial -3- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Ke y Issues
• Estimate Frequency Response Functions (FRFs) Suit-able for Modal Parameter Estimation
• Minimiz e Digital Signal Processing Errors (Leak-ag e!)
• Minimiz e Small Structural Nonlinearities
• Multiple Reference FRF Data
• Frequency Rang e and Resolution
Excitation Tutor ial -4- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Basic Assumptions
• Linearity
• Time Invariance (Stationarity, Consistency)
• Obser vability
• Reciprocity
Error Considerations
• Variance Error: Averaged value equals expected value
• Bias Error: Averaged value not equal to expected value
Excitation Tutor ial -5- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Test Object Configuration
• Fixed Boundary Conditions
• Free Boundary Conditions
• Shock Cord
• Foam Rubber
• Air Suspension
• Realistic Boundary Conditions
• Match Impedance(s) at Boundaries
• Mass Loaded Boundary Conditions
Excitation Tutor ial -6- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Other Test Configuration Considerations
• Test Fixturing
• Interaction with Test Object
• Test Object
• Number of References
• Fixed Excitation/Response Locations
• Location of References (Shakers)
Excitation Tutor ial -7- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Instrumentation
• Shaker Type (electromagnetic, hydraulic, etc.)
• Shaker Control Capability (force matching vs. mo-tion matching)
• Specifications
• Force Amplitude Range (static vs. static + dy-namic)
• Frequency Rang e
• Signal Source (noise, DAC, etc.)
Excitation Tutor ial -8- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Physical Connections - Shaker to Structure
• Mount Force Transducer on Test Object (glue, screw,vacuum, etc.)
• Connect Force Transducer to Shaker with Stinger (quill,etc.)
• Stiff in Direction of Excitation
• Weak in Transverse Directions
• No Moments or Side Loads on Force Transducer
• No Moments or Side Loads on ShakerMinimiz e Shaker Fixture Motion/Resonances
Excitation Tutor ial -9- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Data Quality Issues
• Force Level (High/Low Amplitude , Improper FrequencyContent)
• Loose Exciter Connection (Stinger)
• Load Cell, Shaker Connection Not Perpendicular to TestObject
• Load Cell Not Aligned with Response Transducer atConnection
• Low Batter y Po wer in Transducer Signal Conditioning
• Loose Cable Connections
• Cables Vibrating, Bad or Intermittent Cables
• Electrical and/or Radio Frequency Noise on Data
• Ground Loop
• 50/60 Hertz Noise
• Rattles in Test Object
• Unmeasured Inputs
Excitation Tutor ial -10- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Data Quality/Consistency
• Monitor Typical Measurements
• Frequency Response Functions for Noisy Data,Rattles, Frequency Shifts, Amplitude Changes
• Driving Point Frequency Response Function
• Cross Point Frequency Response Function
• Reciprocity Check
• H pq = Hqp
• Monitor Force Spectrum of Each Input
• Equipment Failure , Loose Stinger(s)
• Monitor Force Correlation Characteristics for MultipleInputs
Excitation Tutor ial -11- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -12- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -13- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -14- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -15- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -16- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -17- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -18- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -19- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -20- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -21- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -22- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -23- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -24- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -25- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Test Set-Up Examples
Excitation Tutor ial -26- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Excitation Signal Considerations
The type of excitation signal used to estimate frequency re-sponse functions depends upon several factors. Generally,the excitation signal is chosen in order to minimize noisewhile estimating the most accurate frequency response func-tion in the least amount of time. With the advent of the FFT,excitation signals are most often contain broadband frequen-cy information and are limited by the requirements of the FFT(totally obser ved transients or periodic functions with re-spect to the observation window).
Excitation Tutor ial -27- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Classification of Excitation Methods
• Steady State
• Slow Swept Sine
• Stepped Sine
• Random
• True Random
• Periodic
• Fast Sine Sweeps
• Pseudo Random
• Periodic Random
• Transient
• Burst Random
• Impact
• Operating
Excitation Tutor ial -28- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Excitation Signal Characteristics
RMS to Peak Ratio - This ratio is formed by taking the RMSvalue of the excitation signal over the observation timeperiod (T) compared to the largest value (positive ornegative) in the time period (T). Generally, good excita-tion signals have larger RMS to peak ratios.
Signal to Noise Ratio - This ratio is formed by taking the RMSvalue of the excitation signal over the observation timeperiod (T) over the RMS value of the noise over thesame time period (T). Generally, good excitation signalshave larger signal to noise ratios.
Distortion - Distor tion refers to the ability of the excitationsignal, when averaged, to allow nonlinear characteris-tics in the data to be preserved. Generally, since experi-mental modal analysis is a linear process, excitationsignals that minimize distor tion are considered more fa-vorably. Nonlinear characteristics must be identified byother experimental or analytical techniques.
Excitation Tutor ial -29- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Excitation Nomenclature
In order to explain the way in which excitation signals arecreated and sent to the shaker, par ticularly in random test-ing, a number of nomenclature issues must be explained.
Delay Blocks - The number of contiguous blocks of excitationthat take place without the associated input and outputdata being acquired are referred to as the delay blocks(Nd ).
Capture Blocks - The number of capture blocks refers to thenumber of contiguous blocks of time data (excitation(input) and response (output)) that are recorded or cap-tured for each average ( Nc).
Av erage (Ensemble) - The average or ensemble refers to thetotal collection of contiguous time blocks that con-tribute to each power spectral average . The total timeof each average is equal to the sum of the number ofdelay blocks ( Nd ) plus the number of capture blocks(Nc) times the observation period (T) which is the samefor all delay and capture blocks.
Burst Length - Burst length is the percentage (0 to 100%) ofthe average or ensemble time that the excitation signalis present.
Excitation Tutor ial -30- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Excitation Nomenclature
Po wer Spectral Averages - The number of power spectral aver-ag es (Navg or Na) is the number of auto and cross spec-tra that are averaged tog ether to estimate the FRF mea-surements.
In order to clarify the preceding terminology, the followingfigure is a schematic representation of the number of con-tiguous blocks of time domain data contributing to one pow-er spectral average . In this example , the two blocks marked"D" represent delay blocks and the four blocks marked "C"represent capture blocks. The total time for each powerspectral average is, therefore , six contiguous blocks of timedata (6 × T seconds of data).
Burst Length (%)0 100
2 3 4 5
Window Function
60 1
Number of Contiguous Time Blocks (6T)
D D C C C C
Total Contiguous Time Per Power Spectral Average
Excitation Tutor ial -31- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Random Excitation Methods
Typical Random Excitation Test Setup
Excitation Tutor ial -32- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pure Random
• Advantages:
• Fair general excitation type
• Fair signal to noise ratio
• Fair RMS to peak ratio
• Reduces distortion
• Good measurement test time
• Works well with Zoom
• Disadvantages:
• Leakage a serious problem
• More averages required
• Poor characterization of non-linearities
• Typical DSP Window
• Hanning Window
Excitation Tutor ial -33- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pure Random
0 5 10 15 20 25 3010
−3
10−2
10−1
100
101
Spectral line (bin)
Magn
itude
Power Spectrum − Pure Random
Signal Energy Content - Pure Random
Excitation Tutor ial -34- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pure Random
Typical Random Signal - Time Domain
0 0.5 1 1.5 2 2.5 3 3.5 4−1
−0.8
−0.6
−0.4
−0.2
0
0.2
0.4
0.6
0.8
1
Time (Seconds)
Am
plitu
de
Random Force
Excitation Tutor ial -35- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pure Random
Typical Random Signal - Frequency Domain
0 10 20 30 40 50 60 70 80 90 100−0.5
0
0.5
Frequency (Hertz)
Rea
l Par
t
Random Force
0 10 20 30 40 50 60 70 80 90 100−0.5
0
0.5
Frequency (Hertz)
Imag
inar
y P
art
Excitation Tutor ial -36- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pure Random
Typical Random Signal - Frequency Domain
0 10 20 30 40 50 60 70 80 90 10010
−2
10−1
100
Frequency (Hertz)
Mag
nitu
de
Random Force
0 10 20 30 40 50 60 70 80 90 100−200
−100
0
100
200
Frequency (Hertz)
Pha
se (
Deg
)
Excitation Tutor ial -37- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pure Random
Typical Random Signal - Frequency Domain
0 10 20 30 40 50 60 70 80 90 10010
−2
10−1
100
101
102
Frequency (Hertz)
Mag
nitu
de
Random Force−Averaged
0 10 20 30 40 50 60 70 80 90 100−200
−100
0
100
200
Frequency (Hertz)
Pha
se (
Deg
)
Excitation Tutor ial -38- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pseudo Random
A pseudo random excitation signal is a random time domainsignal that is constructed from a limited sequence of randomnumbers. Conventionally, the pseudo random excitation sig-nal is constructed in the frequency domain with a uniformamplitude , random phase spectrum at the discrete frequen-cies of the measurement. Therefore , a single time block ofthe pseudo random excitation signal has energy at all fre-quencies of the measurement.
• Advantages:
• Minimum leakage
• Fair signal to noise ratio
• Fair RMS to peak ratio
• Good measurement test time
• Disadvantages:
• Non-linear systems generate periodic noise
• Typical DSP Window
• Uniform Window
Excitation Tutor ial -39- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pseudo Random
0 5 10 15 20 25 3010
−3
10−2
10−1
100
101
Spectral line (bin)
Magn
itude
Power Spectrum − Pseudo Random
Signal Energy Content - Pseudo Random
The pseudo random excitation signal is applied to the exciterrepetitively. While the excitation signal is periodic in the ob-ser vation window (T), the response will not become periodicuntil the startup transient has decayed to zero. At this time,one or more averages are taken.
Excitation Tutor ial -40- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pseudo Random
Typical Pseudo Random Signal - Frequency Domain
0 10 20 30 40 50 60 70 80 90 100−1
−0.5
0
0.5
1
Frequency (Hertz)
Rea
l Par
t
Psuedo−Random Force
0 10 20 30 40 50 60 70 80 90 100−1
−0.5
0
0.5
1
Frequency (Hertz)
Imag
inar
y P
art
Excitation Tutor ial -41- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pseudo Random
Typical Pseudo Random Signal - Frequency Domain
0 10 20 30 40 50 60 70 80 90 10010
−2
10−1
100
101
102
Frequency (Hertz)
Mag
nitu
de
Psuedo−Random Force
0 10 20 30 40 50 60 70 80 90 100−200
−100
0
100
200
Frequency (Hertz)
Pha
se (
Deg
)
Excitation Tutor ial -42- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Pseudo Random
Typical Pseudo Random Signal - Frequency Domain
−1 −0.5 0 0.5 1−1
−0.8
−0.6
−0.4
−0.2
0
0.2
0.4
0.6
0.8
1
Real Part
Imag
Par
t
Psuedo−Random Force
Excitation Tutor ial -43- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Periodic Random
A periodic random excitation signal is a random time domainsignal that is constructed from an unlimited sequence of ran-dom numbers. Conventionally, the periodic random excita-tion signal is constructed in the frequency domain with a ran-dom amplitude, random phase spectrum at the discrete fre-quencies of the measurement. Therefore , a single time blockof the periodic random excitation signal does not have ener-gy at all frequencies of the measurement.
• Advantages:
• Minimum leakage
• Fair signal to noise ratio
• Fair RMS to peak ratio
• Reduces distortion
• Fair measurement test time
• Disadvantages:
• Slower than other periodic excitations
• Special hardware needed
• Typical DSP Window
• Uniform Window
Excitation Tutor ial -44- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Periodic Random
0 5 10 15 20 25 3010
−3
10−2
10−1
100
101
Spectral line (bin)
Magn
itude
Power Spectrum − Periodic Random
Signal Energy Content - Periodic Random
The periodic random excitation signal is applied to the ex-citer repetitively; while the excitation signal is periodic in theobser vation window (T), the response will not become peri-odic until the startup transient has decayed to zero. After suf-ficient time has elapsed to allow for both the input and outputto become periodic, the first average of data is taken. Thisprocess is repeated until sufficient averages have been tak-en.
Excitation Tutor ial -45- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Burst Random
• Advantages:
• Good general excitation
• Minimum leakage
• Fair signal to noise ratio
• Fair RMS to peak ratio
• Reduces distortion
• Good measurement test time
• Disadvantages:
• Special hardware needed
• Voltage feedback excitation amplifier
• Typical DSP Window
• Uniform or Exponential Window
Excitation Tutor ial -46- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Burst Random
0 5 10 15 20 25 3010
−3
10−2
10−1
100
Spectral line (bin)
Magn
itude
Power Spectrum − Burst Random
Signal Energy Content - Burst Random
Excitation Tutor ial -47- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Burst Random
Exciter Systems:
Exciter systems, particularly electromagnetic, attempt tomatch the excitation signal to some physical characteristic ofthe exciter. Typically, this means that the displacement, ve-locity or acceleration of the armature of the shaker will at-tempt to match the excitation signal. Note that this is nor-mally an open loop control process; no attempt is made toexactly match the excitation signal.
Voltage Feedback:
Voltage feedback refers to the types of amplifiers in the ex-citer system that attempt to match the voltage supplied to theshaker to the excitation signal. This effectively means thatthe displacement of the armature will follow the excitationsignal. Therefore , if a zero voltage signal is sent to the ex-citer system, the exciter will attempt to prevent the armaturefrom moving.
Current Feedback:
Current feedback refers to the types of amplifiers in the ex-citer system that attempt to match the current supplied to theshaker to the excitation signal. This effectively means thatthe acceleration of the armature will follow the excitation sig-nal. Therefore , if a zero voltage signal is sent to the excitersystem, the exciter will allow the armature to move , prevent-ing any force to be applied by the exciter system.
Excitation Tutor ial -48- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Burst Random
Signal to shaker
500 1000 1500 2000-1.5
-1
-0.5
0
0.5
1
1.5
Signal from load cell (Voltage Feedback)
500 1000 1500 2000-1.5
-1
-0.5
0
0.5
1
1.5
Signal from accelerometer
500 1000 1500 2000-6
-4
-2
0
2
4
6x 10
-3
Excitation Tutor ial -49- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Hybrid Random Excitation Methods
Several random excitation methods have recently beendemonstrated that are hybrid methods involving combina-tions of burst random and pseudo random, burst random andperiodic random together with cyclic averaging.
0 5 10 15 20 25 3010
−3
10−2
10−1
100
101
Spectral line (bin)
Magnitu
de
Power Spectrum − Burst Pseudo Random
Signal Energy Content - Burst Pseudo Random
0 5 10 15 20 25 3010
−3
10−2
10−1
100
101
Spectral line (bin)
Magnitu
de
Power Spectrum − Burst Periodic Random
Signal Energy Content - Burst Periodic Random
Excitation Tutor ial -50- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Summary of Excitation Signal Choices
Excitation Signal Characteristics
Steady Pure Pseudo Random Periodic Impact Burst
State Random Random Chirp Random
Sine
Minimize Leakage No No Yes Yes Yes Yes Yes
Signal-to-Noise Ratio Very Fair Fair Fair High Low Fair
High
RMS-to-Peak Ratio High Fair Fair Fair High Low Fair
Test Measurement Time Very Good Ver y Fair Fair Ver y Very
Long Short Shor t Shor t
Controlled Frequency Content Yes Yes Yes Yes Yes No Yes
* * * * *
Controlled Amplitude Content Yes No Yes No Yes No No
* *
Removes Distortion No Yes No Yes No No Yes
Characterize Nonlinearity Yes No No No Yes No No
* Special Hardware Required
Excitation Tutor ial -51- Febr uary 5, 2001
Str uctural Dynamics Research Laborator yUniversity of Cincinnati
Shaker Excitation for Experimental Modal Analysis
Summary/Conclusions/Discussion
Excitation Tutor ial -52- Febr uary 5, 2001