Upload
ajdnanthakumar
View
223
Download
0
Embed Size (px)
Citation preview
8/10/2019 MR Fluid MTech Seminar
1/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
VIBRATION CONTROL USING
MAGNETORHEOLOGICAL FLUIDS
AE 694 - M.Tech Seminar
By
NITHIN S NAIR(10301036)
Under the guidance of
Prof. Ms. Mira Mitra
Department of Aerospace Engineering,
Indian Institute of Technology, BombayNovember, 2010
8/10/2019 MR Fluid MTech Seminar
2/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Table of contents
Chapter Page No.
1. Introduction 1
1.1 Smart Materials 1
1.2 Magnetorheological (MR) Fluids 1
1.3 Theory 2
1.4 The Bingham Plastic Model for MR Fluids 3
1.5 Pre-Yield Response 4
1.6 Post-Yield Flow 4
1.7 Carrier Fluids 6
1.8 Other Effects 6
2. Applications of Magnetorheological Fluids 7
2.1 Commercial MR Fluids 7
2.2 Heavy Duty Vehicle Seat Suspensions 7
2.3 Control of Seismic Vibrations in Structures 82.4 Seal-Less Vibration Damper 9
2.5 MR fluids in structural applications 9
3. The Application of MR Damper for Semi-Active Control of
Vehicle Suspension System 11
3.1 Introduction 11
3.2 MR Damper and Parameter Estimation 11
3.3 BOUC WEN Model and Parameters Estimation 13
3.4 Semi-Active Control of Vehicle Suspension System 14
3.5 Discussion 16
4. Seismic Response Control Using Multiple MR Dampers 18
4.1 Introduction 18
4.2 MR damper Modeling 18
4.3 Clipped-Optimal Control Algorithms 19
8/10/2019 MR Fluid MTech Seminar
3/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
4.4 Five Story Structure - Two MR Dampers 21
4.5 Discussion 21
5 Conclusion 23
8/10/2019 MR Fluid MTech Seminar
4/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
List of figures
Figure No. Title Page No.
1.1 A MR fluid under magnetic field 1
1.2 The schematic of off state and on state of MR fluids 2
1.3 Shear stress versus shear strain rate for the Bingham model 3
1.4 Operational modes of MR fluid devices 4
1.5 Shear stress shear strain relationship of MR material 42.1 Rheonetic RD-1001/4 MR Fluid Damper 7
2.2 Schematic of MR Fluid Seismic Damper 8
2.3 Rheonetic RD-1013-1 vibration damper 9
2.4 Three-layered adaptive beam configuration with MR material 10
3.1 Schematic Diagram of the MR Damper 12
3.2 Responses of force vs. time and force vs. displacement underdifferent electric currents 13
3.3 Equivalent damping coefficient vs. velocity under variouselectric currents 13
3.4 Bouc Wen model 14
3.5 Simplified quarter car model 15
3.6 Acceleration response of sprung mass 16
4.1 Simple Mechanical Model of the MR Damper 18
4.2 Graphical Representation of Algorithm for Selecting the
Command Signal 20
4.3 Block Diagram of Semi-Active Control System 21
8/10/2019 MR Fluid MTech Seminar
5/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
ABSTRACT
Vibration control is a set of technical means aimed to reduce the undesired vibrations in a
structure. There are several techniques used in vibration control. Mainly these techniques can
be classified as passive, active and hybrid. Passive methods have no feedback systems, butactive system incorporates real-time recording instrumentation and feedback system to
control vibration. Hybrid is a combination of both active and passive. In this seminar the role
of smart materials, mainly Magnetorheological fluids (MR), is highlighted.
Magnetorheological fluids are those field responsive fluids which change their rheological
properties when a magnetic field is applied. These fluids can be used in structures to reduce
the vibration by changing its damping force using a magnetic field. To study the variation of
properties of a MR fluid, a suitable model should be developed to explain the variation.Several models like Bingham plastic model, Bouc-Wen model etc. has been proposed. This
seminar deals with mainly Bouc-Wen model which is suitable to explain the behaviour of
MR fluid when used in a damper. The MR fluids when used in a damper can be used in
automobile suspensions, aircraft landing gear, seismic vibration damping system etc. In this
report, the role of MR fluids in seismic vibration reduction in buildings and vehicle
suspension is discussed.
8/10/2019 MR Fluid MTech Seminar
6/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
CHAPTER-1
INTRODUCTION
1.1 Smart Materials
Smart materials are those materials which can alter some of their properties on the
application of an external field. Materials exhibiting ferroelectricity, pyroelectricity,
piezoelectricity, a shape memory effect, electrostriction, magnetostriction, electro-chromism,
photomagnetism are some examples. These materials are mostly used in their solid state.
There is another class of s mart materials known as field -responsive fluids which are soft,
typically dispersions or gels, rather than solids. Magnetorheological fluids, electrorheological
fluids, ferrofluids and certain types of polymeric gels are included in this kind. Field
responsive fluids constitute dispersions of particles in a carrier liquid and some aspect of their
rheology can be controlled by an external electric field or magnetic field. In this seminar, the
focus is on Magnetorheological fluids (MR fluids).
1.2 Magnetorheological (MR) Fluids
Magnetorheological fluids come under the category of field-responsive fluids. Their
rheological properties may be rapidly varied by applying a magnetic field. They are
suspensions of particles in inert carrier liquids. When exposed to a magnetic field, the
suspended particles polarize and interact to form a structure aligned with the magnetic
field that resists shear deformation or flow. The particles are of size of the order of 1 to 10
m and these are added to fluids such as mineral oils or silicone oils. The weight fractions of
these particles are large and vary in the range 30% to 50%. MR fluids also contain small
amounts of additives so as to affect the polarisation of the particles and stabilize the
suspension against settling.
Figure 1.1 A MR fluid under magnetic field [9]
8/10/2019 MR Fluid MTech Seminar
7/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
The change in properties of MR fluids is due to the realignment of particles in the fluid to
form fibrils, or long strands of suspended particles, that resist shear. The process of fibration
occurs in a few milliseconds after the application of the field. In the absence of an external
field, MR fluid may be characterized as Newtonian, i.e., resisting shear strain is proportional
to shear stress. But actually, because of the additives they contain and the heavy loading of
solid particles, they act as non-Newtonian even when no field is applied.
1.3 Theory
As explained above the change in properties is due to the realignment of the particles.
This alignment is related to the displacements and torque produced in the medium by the
field and the translational motion and relocation of particles to positions that have local
minimum potential energy. This results in an increase in viscosity and an increase in shear
strength of the material.
When MR fluid flows, or when there is a relative motion between the walls of its
container, shear stress distribution develops across the fluid due to the shear strain occurring
in the fluid. When a magnetic field oriented perpendicular to the direction of flow is applied,
fibrils are formed across the flow, and because of the motion of fluid or the walls these fibrils
are broken and then reformed again. This continuous breaking and reforming of these particle
chains result in a force resisting the motion of the fluid or walls. This results in the formation
of a field-dependent component of shear stress. This component of shear stress is much larger
than the viscous shear stress. This large and controllable shear stress is useful in mechanical
systems. When MR fluid reaches magnetic saturation, the upper limit of the induced shear
stress is reached.
Figure 1.2 The schematic of off state and on state of MR fluids [5]
8/10/2019 MR Fluid MTech Seminar
8/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
1.4 The Bingham Plastic Model for MR Fluids
The formation of the fibrils within the MR fluid br ings only little change in the fluids
viscosity actually. The effect of the fibrils is to produce a shear stress which is independent of
the strain rate [1]. This stress is referred to as yield stress and denoted as y . This term is added
to the general Newtonian model of fluids and the total stress is obtained.
( ) y F is the viscosity of the fluid, is the strain rate of the fluid and is the applied field.
Here yield stress, y is given as a function of the applied field. It is typically proportional to
the field strength raised to a power between 1 and 2. The response by this model is plotted
and shown below. Thus MR fluids are characterized in part by their zero-field viscosity and
field-dependent yield stress.
Figure 1.3 Shear stress versus shear strain rate for the Bingham model [6]
In experiments, the dynamic viscosity, is determined by a linear fitting of a line to
experimental plotted data, and the intersection of this line with the shear stress axis is takenas y . Initiating the motion or flow requires overcoming a static yield stress , y s , and this is
larger than the dynamic yield stress , y d . But this quickly falls to the dynamic value once
motion is there. Once shear stress has reached its dynamic value, it tends to follow the fitted
straight line towards y as decreases. This behaviour may be due to the reattachment to
the walls of the field-induced fibrils, which were broken near their ends by the bulk shear of
the fluid accompanying the flow. Also , y s can rise significantly after long periods of static
state.
8/10/2019 MR Fluid MTech Seminar
9/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Figure 1.4 Operational modes of MR fluid devices [2]
1.5 Pre-Yield Response
The Bingham plastic model proposed that stress less than yield stress y produces no
flow of the fluid; but in real case the fluid responds to stress in this range. Even if y
increases with F , the yield occurs at approximately the same strain, regardless the field
strength. For many purposes MR fluids are regarded as viscoelastic solid.
The shear stiffness of viscoelastic solids are represented by the complex shear modulus*G G jG , where the real part G is called the storage modulus which measures the
materials ability to elastically store strain energy and the imaginary part G is called the loss
modulus which is associated with the dissipation of energy during deformation.
1.6 Post-Yield Flow
Figure 1.5 Shear stress shear strain relationship of MR material [8]
When a magnetic field is applied, only a small portion of the fluid is subjected to the
applied field while the rest is free to flow as a conventional, low viscosity fluid. Two
possibilities are explained to illustrate how shear is created in the fluid [1]. When the fluid is
forced through a gap under pressure or when the confining boundaries move with respect to
8/10/2019 MR Fluid MTech Seminar
10/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
the other, shear may be produced. The gap considered is small in the direction of the field.
This close spacing is required in order to produce a field strong enough to activate the fluid.
If adequate field can be generated, the fibrils will form over a greater distance within the
fluid.
The analysis of the above possibilities can be done with the help of elementary fluid
mechanics. A differential control volume within the fluid shows how the pressure gradient
p produces a shear stress distribution through the fluid layer. This distribution is of the
form
( )2h
z p z
wheredp
p dx = constant and h is the thickness of the gap.
This distribution is independent of the nature of the material in the gap. But as the fluid
exhibits a yield stress, a critical pressure is required for the flow to occur. This critical
pressure is related to the gap geometry and fluid yield stress and is given by
2 y
c
dpdx h
The flow will occur if the pressure exceeds this critical level this flow will be characterized
by shear of a layer near each boundary while the central portion of the fluid remains
unyielding. This resembles a plug flow. The volumetric flow rate can be obtained by
integration of the distribution of velocity across the gap. It gives the result
2
2
2
12
y y p h p hQb p
This result can be written in the non-dimensional form3 2 3* * * *(1 3 ) 4 0 P T P T
where3
*
12
bh p P
Q ,
2
*
12 ybhT
Q
There are approximations which can be done to this equation, depending upon the flow rate.
When*
T > 0.5, the equation becomes* *1 3 P T
and for low flow conditions corresponding to*
T > 200, the approximation is
8/10/2019 MR Fluid MTech Seminar
11/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
* *2
23
P T .
1.7 Carrier Fluids
The carrier liquid in an MR fluid plays a very important role. The function of a carrier
liquid is to provide a liquid in which the magnetically active phase particulates are
suspended. The approximate relative volume fractions of the liquid phase range between 0.5
and 0.9. Silicone oils, synthetic or semi-synthetic oils, mineral oils, lubricating oils and
combination of these can be used as carrier liquids [5]. It is important to consider the boiling
temperature, vapour pressure at elevated temperatures and freezing point while selecting the
carrier liquids. The carrier liquid should also be highly non-reactive toward the components
or materials used in the device. It is important to minimise the off-state viscosity of the
carrier liquid and choose liquids that do not show significant variation in the viscosity at a
given temperature. A new family of material emerged which called MR elastomers replaces
the fluid component by cross-linked material like rubber or silicone. Additives are also
incorporated into MR fluids to enhance their performance and make the fluids and devices
more durable.
1.8 Other Effects
MR fluids give weaker responses to changes in their environment. Temperature variations
affect the fluid predominately through the inert liquid phase of the suspension. The carrier
fluid may expand or contract with temperature changes, affecting the effective volume
fraction of the particles, and its viscosity can also vary with temperature. The influence of
particle volume fraction is studied by using the property, relative viscosity, which is defined
as the ratio of viscosity of the MR suspension to the viscosity of the carrier fluid.
8/10/2019 MR Fluid MTech Seminar
12/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Chapter 2
APPLICATIONS OF MAGNETORHEOLOGICAL FLUIDS
2.1 Commercial MR Fluids
MR fluid caters to various applications depending on the modes used. These range from
automotive to optics and also defence applications. Lord Corporation has commercialized
several MR fluids and various MR fluid based systems including an MR fluid brake for use in
the exercise industry and a controllable MR fluid damper for use in truck seat suspensions.
Most devices that use controllable fluids can be classified as having either fixed poles
(pressure driven flow mode) or relatively moveable poles (direct-shear mode). The basic
composition of these four fluids is given in the table .
Table 2.1 Properties of commercial MR fluids [2]
Some of the significant applications include
2.2 Heavy Duty Vehicle Seat Suspensions
In heavy duty vehicle seat applications, flow mode is employed. Flow mode is usually
applied in Dampers and shock absorbers wherein the fluid is forced across field in a direction
in which movement is to be controlled.
Figure 2.1 Rheonetic RD-1001/4 MR Fluid Damper [2]
8/10/2019 MR Fluid MTech Seminar
13/29
8/10/2019 MR Fluid MTech Seminar
14/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
extended period as a seismic event is often sudden and non-dynamic. MRX -140ND is an
MR fluid used for such a use. This fluid is given a small yield strength which gives it a
greasy consistency preventing the particles from gravitational settling.
2.4 Seal-Less Vibration Damper
Figure 2.3 Rheonetic RD-1013-1 vibration damper [2]
Seal less vibration dampers work in flow mode. A small controllable MR fluid
vibration damper used for industrial application is shown in figure. A small steel disc is
moved in a chamber of MR fluid. Axial motion is primarily achieved producing a
damping force of 0-125N although secondary lateral and flexing motions are also
possible. It uses elastomer rubber elements instead of dynamic sliding seals owing to
relatively small amplitudes. The device can also be used as a locking device.Since the natural rubber diaphragms are not compatible with hydrocarbon oil based
fluids, water based fluids like MRX-242AS are used, which are exceptionally stable due
to the wide choice of surfactants.
2.5 MR fluids in structural applications
Magnetorheological materials are potentially applicable to structures and devices
when a tuneable system response is required [7]. When incorporated into an adaptive
structural system, they can yield higher variations in the dynamic response of the structure.
Magnetorheological (MR) materials, due to their semi-active control capabilities, are
candidate materials, which can cause changes in both damping and stiffness of the structure
simultaneously [8]. Their utilization in these applications is based on the concept of
optimized control with minimum energy addition via semi-active control. The MR fluid layer
is embedded in a laminated composite to control its vibration. The relationship between the
magnetic field and the complex shear modulus of MR materials in the pre-yield regime is
researched using oscillatory rheometry techniques. Vibration characteristics of MR adaptive
structures are predicted for different magnetic field levels by structural dynamic modelling.
8/10/2019 MR Fluid MTech Seminar
15/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Figure 2.4 Three-layered adaptive beam configuration with MR material [8]
A test beam is modelled some principle like the following [8]. The surface plates must be
made of elastic materials, the surface plates should not affect the distribution and strength of
the magnetic field, the MR layer should be uniform between the surface plates, and thefabricated MR test beam should be uniform and straight. Permanent magnets are used to
generate magnetic field over the test beam. Variations in the magnetic field level are obtained
by changing the distance between the permanent magnets by using a simple screw
mechanism.
8/10/2019 MR Fluid MTech Seminar
16/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Chapter 3
THE APPLICATION OF MR DAMPER FOR SEMI-ACTIVECONTROL OF VEHICLE SUSPENSION SYSTEM
3.1 Introduction
Semi-active suspensions can be nearly as effective as fully active suspensions inimproving ride quality and were proposed in the early 1970s. The semi-active suspension can
still work in passive condition even when the control system fails. The semi-active
suspension system combines the advantages of both active and passive suspensions; i.e. it
provides good performance compared with passive suspensions and is economical. It does
not require either higher-power actuators or a large power supply.
A MR damper is designed and fabricated first in this paper. A nonparametric model for the
damper is constructed and parameter estimation is done for the MR damper based on the
experimental results. The model results are compared with those of experimental results. A
car model is established with the model of MR damper and the governing equation is
obtained for the suspension system. Sky-hook control, a semi-active control strategy, is
adopted to control the vibration of suspension system over random road excitation.
Simulation is carried out and results are compared with those of passive suspension. The
potential application of MR damper in vehicle suspension system is proved.
3.2 MR Damper and Parameter Estimation
3.2.1 Design of MR damper and experimental setup
The MR damper used works in flow mode. The damper is218 mm long in its extended
position, and has 25 mm stroke. The main cylinder houses a piston, a magnetic circuit, an
accumulator and MR fluid. MR 132 LD is used in the damper. The MR fluid valve is
contained within the piston and consists of an annular flow channel with 1.5 mm gap. The
magnetic field is applied radially across the gap, perpendicular to the direction of fluid flow.
The total axial length of the flow channel is 6 mm which exposed to the applied magnetic
field. Viscosity of MR fluid in the valve will be increased by increasing the electric current
through the electromagnet, thus resisting the MR fluid flow through the valve and increasing
the damping force of the MR damper.
The property of the damper should be determined first and then a model must be developed
that can accurately reproduce the behaviour of the MR damper in order to apply the MR
damper in vibration control of vehicle suspension system. To determine the property of the
MR damper an experimental test rig is set up. This set up also helps in obtaining the dynamic
data necessary for estimating the parameters of the model. A computer-controlled INSTRON
8/10/2019 MR Fluid MTech Seminar
17/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Test Machine (Model 8874) is used and the MR damper is fixed in it. The INSTRON Test
Machine has a load cell and a displacement sensor in it to measure the force produced by the
MR damper and the displacement of the piston. Two types of excitations, sinusoidal and
triangular, are used. The excitation frequencies are 1, 2 and 4 Hz and the amplitudes of
excitation are 1, 2 and 4 mm, respectively.
Figure 3.1 Schematic Diagram of the MR Damper [4]
The applied electric current is from 0 to 1 A with increment of 0.25 A. The force and
displacement responses of the damper are sampled simultaneously by the computer via an
A/D converter. The excitation signal is also produced by the computer and sent out to the
hydraulic actuator via a D/A converter. Velocity response can be obtained by differentiating
the displacement. All experiments are carried out at the room temperature of 23 C.
3.2.2 Experimental Results
The effect of the magnetic field on damping force is studied by applying 1 Hz excitation
under five constant electric currents. The result obtained is shown in the figure. With the
increasing of the applied electric current, the damping force will increase remarkably,
however when the applied electric current is more than 0.75 A, the increase of the damping
force is no longer significant. This means that saturation of the MR effect occurs at 0.75 A.
The force produced by the damper is not exactly centred at zero. This is due to the presence
of highly compressed air in the accumulator in the MR damper and the existence of air in the
cylinder which occupies among the MR fluid. The maximum force of MR damper at 1 A is
approximately equal to eight times of that without electric field. Experiments are done with
triangular excitation to obtain the relation of equivalent damping coefficient to velocity and
electric current. The equivalent damping coefficient of the damper against velocity under
various electric currents is shown in figure. From the figure, at low velocity, equivalent
damping coefficient will increase significantly.
8/10/2019 MR Fluid MTech Seminar
18/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Figure 3.2 Responses of force vs. time and force vs. displacement under different electric
currents [3]
As the velocity increases, the equivalent damping coefficient under high electric current
decreases rapidly whereas that without electric current decreases slowly. At high velocity, the
effect of current on equivalent damping coefficient is also not so significant. This
phenomenon means that the MR damper cannot be treated as a viscous damper under high
electric current.
Figure 3.3 Equivalent damping coefficient vs. velocity under various electric currents [3]
From the experiments, it is seen that the designed MR damper has very large changeable
damping force range under magnetic field, although the saturated magnetic field is not so big.
Since the MR damper cannot be treated as a viscous damper under high electric current, a
suitable model is necessary to be developed to describe the MR damper.
3.3 BOUC WEN Model and Parameters Estimation
The model of the MR damper should be continuous in all the ranges and be numerically
8/10/2019 MR Fluid MTech Seminar
19/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
tractable for application of MR damper in vibration control. The Bouc-Wen model is adopted
here. The schematic of the model is shown in the figure. The force in this system is given by
0 0 F c x k x z ,
where the evolutionary variable z is governed by1n n
z x z z x z Ax ,
where , and A are parameters related to the shape of hysteresis loop.
These parameters are adjusted to control the linearity in the unloading and the smoothness of
the transition from the pre-yield to the post-yield region.
To estimate the parameters of the model, an error function is introduced as an objective
function
21
N ei pi
i
J F F ,
Where e F is the experimental damping force, p F is the estimated damping force and N is
the number of experimental data. The parameters are calculated. It is seen that the estimated
model can capture the properties of the MR damper except at the region where the velocity is
near zero. So the Bouc Wen model can be used to characterize the property of the MR
damper.
Figure 3.4 Bouc Wen model [3]
3.4 Semi-Active Control of Vehicle Suspension System
3.4.1 Vehicle suspension model
A simple quarter car installed with a MR damper in the suspension system is used. It is
shown in the figure. This is a two-degrees-of-freedom system, mass 2m represents the sprung
8/10/2019 MR Fluid MTech Seminar
20/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
mass while mass 1m means the unsprung mass; 2k represents the stiffness of suspension
system and 1k means the stiffness of tire. The property of the MR damper is determined by
the force equation of the Bouc-Wen model. 0 x is the road excitation. The governing equation
of quarter car model can be obtained by the dynamic analysis as
1 1 0 2 1 2 2 1 1 1 0( ) ( ) ( )m x c x x k x x k x x z ,
2 2 0 2 1 2 2 1( ) ( )m x c x x k x x z ,
where the evolutionary variable z is governed by1
2 1 2 1 2 1( ) ( )n n
z x x z z z x x A x x .
Figure 3.5 Simplified quarter car model [3]
T
1 2x x x
Then the governing equation can be written in the matrix form as
x Cx Kx Fy
where
C
0 0
1 1
0 0
2 2
c cm m
c cm m
, K
1 2 2
1 1
2 2
2 2
k k k
m m
k k
m m
, F
1
1 2
2
0
a k
m m
a
m
and T0y z x .
Let T
X x x . Then the governing equation can be written in the state space as
X AX Bu
where
8/10/2019 MR Fluid MTech Seminar
21/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
C K A
I 0
,F 0
B0 0
, and Tu y 0 0
3.4.2 Control Strategy
The state variables are the relative velocity between the sprung mass and the unsprungmass, as well as the velocity of sprung mass. When the relative velocity between sprung mass
and unsprung mass is in the same direction of the velocity of sprung mass, an electric current
is applied to the MR damper, otherwise no damping force is required. But for MR damper it
is impossible to provide a zero force, so we should minimize the semi-active damping force
without any electric current. So semi-active sky-hook control policy can be described using
the form
2 2 1
2 2 1
( ) 0 Max,
( ) 0 Min.
x x x F
x x x F
3.4.3 Simulation Results
The results show the acceleration response of sprung mass under different control
strategies. The suspension travel response around the body resonance is reduced significantly
under constant control and semi-active control, but they are unable to reduce the suspension
travel response around the wheel hop.
Figure 3.6 Acceleration response of sprung mass [3]
8/10/2019 MR Fluid MTech Seminar
22/29
8/10/2019 MR Fluid MTech Seminar
23/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
CHAPTER 4
SEISMIC RESPONSE CONTROL USING MULTIPLE MR DAMPERS
4.1 Introduction
Magnetorheological (MR) dampers can be implemented as semi-active control devices
for seismic response reduction. For this purpose a clipped-optimal control algorithm based on
acceleration feedback was proposed. So a linear optimal controller was designed and
combined with a force feedback loop to determine the appropriate command voltage to send
to the MR damper. This investigation demonstrates that the MR damper, combined with the
clipped-optimal control algorithm, is effective for controlling a multi-story structure with
multiple MR dampers.
4.2 MR damper Modelling
The damper is 21.5 cm long in its extended position, and the main cylinder is 3.8 cm in
diameter. The main cylinder houses the piston, the magnetic circuit, an accumulator and 50
ml of MR fluid, and the damper has a 25 cm stroke. the magnetic field produced in the
device is generated by a small electromagnet in the piston head. The current for the
electromagnet is supplied by a linear current driver, which generates a 0 1 amp current that is
proportional to an applied DC input voltage in the range 0 3 V. The peak power required is
less than 10 watts. Forces of up to 3000 N can be generated with the device. A simple
mechanical idealization of the MR damper depicted below.
Figure 4.1 Simple Mechanical Model of the MR Damper [4]
The force predicted by this model is given by
8/10/2019 MR Fluid MTech Seminar
24/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
0 0 1 0f ( ) ( ) ( ) z c x y k x y k x x
where the evolutionary variable is governed by1
( ) ( )n n
z x y z z x y z A x y
and
0 00 1
1( ) y z c x k x y
c c
Here, 1k is the accumulator stiffness, the viscous damping observed at larger velocities by 0c .
A dashpot, represented by 1c , is included in the model to introduce the nonlinear roll-off that
was observed in the experimental data at low velocities, 0k is present to control the stiffness
at large velocities, and x0 is the initial displacement of spring 1k
associated with the nominaldamper force due to the accumulator. By adjusting the parameters of the model , and A,
one can control the shape of the hysteresis loops for the yielding element.
The dependence of the force on the voltage applied to the current driver and the resulting
magnetic field can be accounted by
( ) a bu u , 1 1 1 1( ) a bc c u c c u , 0 0 0 0( ) a bc c u c c u
where u is given as the output of a first-order filter given by
( )u u v
and v is the commanded voltage sent to the current driver. This equation is necessary to
model the dynamics involved in reaching rheological equilibrium and in driving the
electromagnet in the MR damper.
4.3 Clipped-Optimal Control Algorithm
Since semi-active control devices are inherently stable, high authority control strategies
may be designed and implemented. But, because these devices are intrinsically nonlinear,
appropriate nonlinear control algorithms must be developed to make use of their uniquecharacteristics. In addition, in determining the control action, the control algorithms should
use readily available measurements. A clipped-optimal controller based on acceleration
feedback was proposed and turned out to be effective for controlling a structure with a single
MR damper. This control algorithm is extended to consider the case in which multiple control
devices are employed to control a structure.
Consider a seismically excited structure controlled with n MR dampers. It is assumed that the
forces provided by the MR dampers are adequate to keep the response of the primarystructure from exiting the linear region, and then the equations of motion can be written as
8/10/2019 MR Fluid MTech Seminar
25/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
z Az Bf Ex g
Where x g
is a one-dimensional ground acceleration, 1 1f f f .... f n is the vector of
measured forces generated by the MR dampers, and z is the state vector. The measurement
equation is given by
y Cz Df n
where y is the vector of measured outputs, and n is the measurement noise vector. In this
application, the measurements typically available for control force determination include the
acceleration of selected points on the structure, the displacement of the MR dampers and the
measurement of the control forces provided by the MR dampers.
Consider the ith MR damper used to control the structure to discuss the algorithm used for
determining the control action. The response of the MR damper is dependent on the relative
structural displacements and velocities at the point of attachment of the damper, and so the
force generated by the MR damper cannot be commanded; only the voltage iv applied to the
current driver for the ith MR damper can be changed directly. To induce the MR damper to
generate approximately the corresponding desired optimal control force ci f , the command
signal iv is selected as follows. When the ith MR damper is providing the desired optimal
force (i.e., i ci f f ), the voltage applied to the damper should remain at the present level. If
the magnitude of the force produced by the damper is smaller than the magnitude of the
desired optimal force and the two forces have the same sign, the voltage applied to the
current driver is increased to the maximum limit so as to increase the force produced by the
damper to match the desired control force. Otherwise, the commanded voltage is set to zero.
This algorithm is graphically represented the figure below.
Figure 4.2 Graphical Representation of Algorithm for Selecting the Command Signal [4]
8/10/2019 MR Fluid MTech Seminar
26/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
The proposed control strategy does not require a model for the MR damper, although the
model of the MR damper is important to system analysis. This is one of the attractive features
of this control strategy.
Figure 4.3 Block Diagram of Semi-Active Control System [4]
4.4 Five Story Structure - Two MR Dampers
Sometimes it is not only important to ensure that the structure is not damaged, but the
contents as well (e.g. sensitive computer or laboratory equipment). To ensure this, the
absolute accelerations of the floors of the structure where this equipment is situated must beminimized. Therefore, the focus of this example is to demonstrate that a high reduction in the
floor accelerations can be achieved while simultaneously maintaining a significant reduction
in the inter-story displacements. In this example, the nominal linear controller was designed
by weighting the absolute acceleration of the top floor of the structure.
Two MR dampers are employed to control a five story structure. The first MR damper is
attached between the base and first floor of the structure (providing control force 1 f ), and
the second is attached between the first and second floors of the structure (providing controlforce 2 f ). Two floors with the same mass, stiffness, and damping were added to the three-
story structure to form the five story structural model. The measurements used for feedback
include the absolute accelerations of the five floors of the structure, and the displacements of
both MR dampers.
4.5 Discussion
The performance of the semi-active control system is compared to that of two passive
systems. Since the properties of the MR damper can be varied dynamically, the semi-activesystems achieved greater response reduction than either of the two passive cases.
8/10/2019 MR Fluid MTech Seminar
27/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
Additionally, the semi-active control systems using the MR damper were shown to be
effective at reducing both the structural displacements and accelerations. The results of this
study are that it is possible to achieve large reductions in the floor while simultaneously
achieving a significant reduction in the inter-story displacements.
8/10/2019 MR Fluid MTech Seminar
28/29
Downloaded from DSpace www.aero.iitb.ac.in/dspace || Deparment of Aerospace Engineering, IIT Bombay
CHAPTER 5
CONCLUSION
MR fluids and devices have made considerable progress towards commercialisation.
Adaptive control devices implementing MR dampers are one of the most promising semi-
active devices for use in vibration control applications. These are used to produce the
required forces in a very short interval of time and help to make a damaged structure behave
like an undamaged structure. The semi-active systems using MR damper achieves greater
response reduction than passive systems because of the dynamically variable MR fluid
properties. MR damper has a very broad changeable damping force range under magnetic
field and the damping coefficient increases with the electric current. These systems using MR
damper are very effective in reducing both the structural displacements and accelerations.
There are still challenges in this area. The major challenge lies in the durability of MR
fluids and the devices with the same. Higher and lower temperature performance of MR
fluids over larger periods of time is also a concern. Also each MR fluid based device is
unique and will therefore need a specially formulated MR fluid. The damping force decreases
with the increase in the excitation amplitude. Under electric current, the MR damper cannot
be treated as a viscous damper and the property of the damper can be described by the Bouc-
wen model.
8/10/2019 MR Fluid MTech Seminar
29/29
References
[1] A. V. Srinivasan and D. Michael McFarland, Smart Structures - Analysis and Design,
The press syndicate of the University of Cambridge, United Kingdom, 2001
[2] Mark R. Jolly, Jonathan W. Bender, and J. David Carlson, Properties and Applications of
Commercial Magnetorheological Fluids , Thomas Lord Research Centre, Lord Corporation,
405 Gregson Drive Cary, NC 27511, SPIE 5th Annual Int. Symposium on Smart Structures
and Materials, San Diego, CA, 15 March, 1998
[3] G.Z. Yao, F.F. Yap, G. Chen, W.H. Li, S.H. Yeo , MR damper and its application for
semi- active control of vehicle suspension system, School of Mechanical & Production
Engineering, Nanyang Technological University, 50 Nanyang Avenue, Singapore 639798,
Singapore
[4] S.J. Dyke1 and B.F. Spencer, Jr., Seismic Response Control Using Multiple MR
Dampers, Dept. of Civil Engineering Washington University, St . Louis, MO 63130, U.S.A.
2Dept. of Civil Engineering and Geol. Sci., University of Notre Dame, Notre Dame, IN
46556, U.S.A.
[5] Dr. Pradeep P. Phul, Magnetorheological (MR) fluids: Principles and applications,
Department of Materials Science & Engineering, University of Pittsburgh, and New Age
Materials Inc, Pittsburgh, PA, USA
[6] Mel Schwartz, Encyclopaedia of SMART MATERIALS, Volume 1 and Volume 2 ,
Wiley-Interscience Publication, 2002
[7] Tjahjo Pranoto, Kosuke Nagaya, Atsushi Hosoda, Vibration suppression of plate using
linear MR fluid passive damper , Department of Mechanical Engineering, Gunma
University, Kiryu, Gunma 376-8515, Japan, Journal of Sound and Vibration 276 (2004) 919
932
[8] Qing Sun, Jin-Xiong Zhou, Ling Zhang , An adaptive beam model and dynamiccharacteristics of Magnetorheological materials , Department of Engineering Mechanics,
Xian Jiaotong Un iversity, Xian Ning Road 28, Xian 710049, China, Journal of Sound and
Vibration 261 (2003) 465 481
[9] http://avcdefense.com/development/