Active Vibration Control for a Cantilevered Beam
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Transcript Active Vibration Control for a Cantilevered Beam
Embedded Control of
Smart Structures
Mid-Summer Presentation By:
Alicia Vaden (Tennessee Technological University)
Graduate Advisor:
Tao Tao
Faculty Advisor:
Ken Frampton, PhD
Objectives
Model and analyze the
vibration response of a
cantilevered beam.
Design a smart materialbased controller that will
reduce the vibrations of
the beam.
Piezoelectric Patch
Implementation
Theory
of project
Building a smart structure
Matlab/Simulink with dSPACE
Initial Displacement Disturbance
White Noise Disturbance
Smart Structures
Ordinary structure with sensory network
Sensors
Actuators
Smart Materials
Piezoelectri
Material
Aluminum Alloy 2024-T4
Cost efficient
Modulus of elasticity
PL3
v ( L)
3EI
E = 73.1 GPa
Exaggerated movements
Vibration
A rapid linear motion of a particle about an
equilibrium position
Undesirable
Stress
Energy loss
Reduce vibration!
Underdamped System
Given initial displacement or force,
oscillates until transition state is reached
Damping ratio, ζ , represents the amount
of damping in a system
0<ζ<1
Modeling Beam
Many different equations and strategies
Transfer Function
Natural Frequency, ωn
Damping ratio, ζ
n
G 2
2
s 2 n s n
2
Modeling Beam from Graph
n
G 2
2
s 2 n s n
2
• From the graph of the
sinusoid, the period,
T,
can be found.
T = 0.14 seconds
With period now known,
the natural frequency
1
f
can be calculated T
Exponential Decay
c(t ) e
nt
sin(nt )
Exponential Decay and ζ
Equation of vibration ignoring sine
a(t ) c1e
nt
Natural frequency, ωn , never changes
To increase exponential decay, increase ζ
Modeled Beam
With ωn and ζ known, the
equation can just be plugged in.
2 x 103
G( s) 2
s 1.5s (2 x 103 )
Implementation
Theory of project
Building
a smart structure
Matlab/Simulink with dSPACE
Initial Displacement Disturbance
White Noise Disturbance
Building Smart Structure
1.
2.
3.
4.
5.
Cut beam to desired length (24”)
Clean attaching area with ethyl alcohol
Use epoxy for insulating area, let cure
Attach copper tape to negative side
Use epoxy to attach piezoelectric, keeping
edges down
6. Remove excess tape and epoxy
7. Solder wires to respective side
Implementation
Theory of project
Building a smart structure
Matlab/Simulink
with dSPACE
Initial Displacement Disturbance
White Noise Disturbance
dSPACE with Matlab
Using a block diagram designed in
Simulink, code is generated
Real-Time Workshop in Matlab works in
conjunction with the Real-Time Interface in
dSPACE
C code is generated that will run outside of
dSPACE through the physical model
RTI works as interface between Matlab and
dSPACE
Implementation
Theory of project
Building a smart structure
Matlab/Simulink with dSPACE
Initial
Displacement Disturbance
White Noise Disturbance
System Flow Diagram
reference
Feedback
+
-
DAC
Low
Pass
Filter
ADC
Power
Amp
Low
Pass
Filter
acceleration
Piezo
Beam
Sensor
1. Sensor - Accelerometer
Detects acceleration of beam
Outputs voltage
More sensitive than piezoelectric patch
1
2. Signal Conditioner
Provide power to accelerometer
Pre-amplify signal from accelerometer
1
2
3. Butterworth Low-Pass Filter
Filters out outside noise
Cleaner graph
Easier to read and more accurate results
Cut-off frequency of 100 Hz
C1
R1
R2
(dc coupled)
+
C2
1
-
(K-1)R
R
2
3
4. AD17 and Oscilloscope Input 1
With noise filtered out, sample sent into
dSPACE
Runs through gain
Splits to oscilloscope
View input voltage going into dSPACE
Voltage cannot exceed ±10 Volts
1
2
3
4
5. Feedback Gain and Oscilloscope
Input 2
Multiplies sensor signal by gain
During loops, vibrations signal begins to decay
Splits to oscilloscope
Monitor output voltage
Voltage cannot exceed ±10 Volts
1
2
3
4
5
6. Low Pass Filter/Power Amplifier
Filter dSPACE output through low-pass filter
Amplifies voltage from low-pass filter
Since dSPACE voltage cannot exceed ±10 Volts
then signal must be amplified to increase voltage
to piezoelectric
Amplifier calibrated to 15 Volts
1
2
3
4
6
5
7. Actuator – Piezoelectric Patch
Voltage is applied to piezoelectric
Piezoelectric will bend or contract to apply
control force to beam
Reduces beam vibrations
1
2
3
7
4
6
5
Closed Loop Feedback
The loop has reached its beginning, thus the
process begins again until the beam has
stopped vibrating
1
2
Closed Loop
3
7 Feedback
Control
System
4
6
5
Results
Tested beam with gains
Positive feedback gains made the beam
unstable
Negative feedback gains proved to be the
best control thus far
Higher gains proved to be most effective
Results
Beam vibration without controller
ζ = 0.0168
Results
Beam vibration with -3 feedback gain applied,
followed by 15 Volt amplification
ζ = 0.05
Results
Beam vibration with - 3 feedback gain applied,
followed by 15 Volt amplification
Aqua sine wave
decays considerably
faster
With gain applied,
beam vibration is
controlled
Implementation
Theory of project
Building a smart structure
Matlab/Simulink with dSPACE
Initial Displacement Disturbance
White
Noise Disturbance
System Flow Diagram
White Noise
(disturbance)
reference
Feedback
+
-
DAC
Low
Pass
Filter
ADC
Power
Amp
Low
Pass
Filter
acceleration
Piezo
Beam
Sensor
White Noise
Before disturbance depended on displacement
White noise is produced by a stimulus containing all
frequencies of vibration.
frequency range limited from 0 to 100 Hertz
magnitude will be ± 10 Volts.
Beam
Extra piece of piezoelectric added to side
completely opposite of actuator.
All previous connections remain the same
New connections
Extra output from dSPACE (white noise)
dSPACE low-pass filter power amplifier beam
Simulink Diagram
??? Voltage-Time domain ???
-3 gain in Simulink
White noise emits random frequencies
Very difficult to determine damping when
viewing from time domain
Frequency Domain
Power Spectral Density Function
describes how the power of a time series is
distributed with frequency
Mathematically, it is defined as the Fourier
Transform of a successive correlation of the time
series
psd command in Matlab
1
f ( )
0 2 (k ) cos(k )
2
k 1
Frequency Domain -3 Gain
Multiple peaks??
Different modes
More than one ωn in beam
2nd order modeling is not most accurate
approach
Power Spectral Density Estimate via Welch
Without Controller
With Controller
-50
Power/frequency (dB/Hz)
-60
-70
-80
-90
-100
40
50
60
70
80
90
Frequency (Hz)
100
110
120
Frequency Domain -3 Gain
First Peak
Very little damping
Controller too weak
Power Spectral Density Estimate via Welch
Without Controller
With Controller
-50
Power/frequency (dB/Hz)
-60
-70
-80
-90
-100
40
50
60
70
80
90
Frequency (Hz)
100
110
120
Increased Power Amplifier to 15V
Dampened white noise by 20 dB
Voltage emitted to piezo approximately 100 V
Piezo is designed to accept the voltage
Repeated high voltage can cause damage
Power Spectral Density Estimate via Welch
-50
Without Controller
With Controller
-55
-60
Power/frequency (dB/Hz)
-65
-70
-75
-80
-85
-90
-95
20
30
40
50
60
70
80
Frequency (Hz)
90
100
110
120
Change Conditions of Beam
Shortening beam by
2 inches changes
results drastically
Placement and
boundary conditions
Proportional
feedback gain
strategy not good
enough for white
noise
-45
-50
-55
Power/frequency (dB/Hz)
Dampens first peak,
but excites second
Power Spectral Density Estimate via Welch
-60
-65
-70
-75
-80
Without Controller
-85
With Controller
30
40
50
60
70
Frequency (Hz)
80
90
100
Future Work
System ID of beam
Design more complicated controller
Bode Plots
Root-Locus Method
Design new circuit
Cut down on wires involved in experiment
Use BNC cables instead of Alligator clips
Less of a hassle
Neater workspace
Questions???
Thank you!!
Embedded Control of
Smart Structures
Mid-Summer Presentation By:
Alicia Vaden (Tennessee Technological University)
Graduate Advisor:
Tao Tao
Faculty Advisor:
Ken Frampton, PhD