amp proposal
TRANSCRIPT
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DEPARTMENT OF ELECTRICALENGINEERING
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Course: INDUSTRIAL PROJECT IVSubject Code: IPR413T (6 MONTHS)
IPR413R (RE-REGISTRATION)
INDUSTRIAL PROJECT PROPOSAL:
ACTIVEMAGNETICBEARINGSby
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Diakiese Ndudi Aubin209024489
A Project Proposal Submitted as a Partial Requirement for theBachelors Degree in Technology (BTech): Electrical Engineering
Control
In the Department of Electrical EngineeringFaculty of Engineering and the Built Environment,
Tshwane University of Technology
Supervisor: Professor Qi Guo-YuanCo-Supervisor:Mr Martial Tatchum
Starting Date:01/08/2013
STUDENTS DETAILS
STUDENT NUMBER: 209024489
TEL. NUMBER: 0762945738
FAX. NUMBER: N/A
CELL. NUMBER: 0762945738
E-MAIL:[email protected]
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PROPOSED TITLE OF PROJECT
ACTIVE MAGNETIC BEARING
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SIGNATURE DATE
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DETAILS OF INTERNAL PROJECT LEADER(Lecturer from TUT, if available)
SURNAME AND INITIALS: Qi G
INSTITUTE:University of Nankai (NKU) ,China
QUALIFICATION:PhD(Control Theory And Control Engineering)
(Nankai,China)
TELEPHONE NUMBER: +27123825385
FAX NUMBER: +27123825003
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SIGNATURE DATE
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DETAILS OF MODERATOR
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INSTITUTE: ..........................................................................................................
QUALIFICATION: ...................................................................................................
TELEPHONE NUMBER: ........................................................................................
FAX NUMBER: ...................................................................................................
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SIGNATURE DATE
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DETAILS OF REPRESENTATIVE
SURNAME AND INITIALS: .................................................................................
INSTITUTE: .........................................................................................................
QUALIFICATION: ..................................................................................................
TELEPHONE NUMBER: .......................................................................................
FAX NUMBER: ..................................................................................................
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SIGNATURE DATE
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Contents
Table of Figures
1. ABSTRACTThe importance of Active Magnetic Bearings (AMB) is becoming more
significant these days in many industrial applications. The AMB system
achieves levitation (free suspension of a moving part in air without any
physical contact), and therefore eliminates any friction and need for
lubrication of the machine. The structure consists of a ferromagnetic rotor
maintained in free space by controlled electromagnetic forces. By doing so,
rotation speeds are much higher; losses and maintenance cost in the system
are significantly reduced.
Although Passive Magnetic Bearings (PMB) is simpler than the AMB in
terms of components (no controller), two main drawbacks are noticed on
that type of Bearing:
Firstly, it is impossible to achieve a six degree of freedom support due
to the restriction of the Earnshaws theorem.
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Secondly, the characteristics of the PMB, compared to the AMB, cannot
be changed easily during the operation. Reason why this project will be
entirely focused on the AMB design and control.
To achieve this purpose, the Active Magnetic Bearings (AMB) consists of
an electromagnet assembly, a set of power amplifiers which supplycurrent to the electromagnets, a controller, and gap(position) sensors
which provide the feedback required to control the position of the rotorwithin the gap. When the process starts, the power amplifier suppliesequal bias current to two pairs of electromagnets on opposite sides of a
rotor. The currents supplied enable the electromagnets to exhibit theirmagnetic forces. As the rotor deviates from its centre position; the
controller will offset the bias currents in order to balance the
perturbations caused by the deviation.
FIGURE : GENERAL DESCRIPTION OF AN ACTIVE MAGNETIC BEARING SYSTEM
2. BACKGROUND ON THE PROJECTNowadays, the use of energy in industrial systems is taken with much care.
The modern trend is to reduce the loss as much as possible in order to
optimize the utilization [2], to reduce the cost and therefore increase the
performance of the systems. Traditional rotary systems were proved to be
very lossy due to the friction[1] caused by the mechanical contact between
the rotor(moving part ) and the electromagnets(stationary part).With the
use of an AMB, frictionless structures are built, allowing most of the energy
delivered to be used efficiently. A magnetic rotor is suspended by an
electromagnet. In order to get an active control of the rotor, its position is
measured by a position sensor. The position signal is then treated by a
controller, which gives a current set point. This signal is then amplified by
the power amplifier, in order to get the necessary actuator current. The
actuator current is the output from a power amplifier, a Pulse Width
Modulated (PWM) signal to be distributed to the actuating electromagnets
for a rectifying force on the position of the levitated ferromagnetic object in
free space.The concept of AMB brings a revolution in aerospace industry
(turbo machinery [7], vacuum technology, machining, and airplane
transportation [2]).
Advantages [9]
Increased energy production
As there is no friction, the operation of classical rotor bearings is
maximized.
http://en.wikipedia.org/wiki/Electromagnethttp://en.wikipedia.org/wiki/Controller_(control_theory)http://en.wikipedia.org/wiki/Electromagnethttp://en.wikipedia.org/wiki/Controller_(control_theory) -
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Reduced losses experienced when transferring energy from one
system to another one.
High energy and fuel consumption
Saving of fuel resources
No pollution and Fire Risk due to lubrication
High circumferential speeds
easily adjustable bearing characteristics
low maintenance cost
Enhanced ability to work at very high temperatures
active vibration control and passing of critical speeds
balancing and unbalance compensation
3. PROBLEM STATEMENTThe magnetic bearings are restricted by the Earnshaws theorem which
clearly states that a collection of point charges cannot be maintained in a
stable stationary equilibrium configuration solely by the electrostatic
interaction of the charges. Instabilities and non linearities are present
because the force exhibited is a function changing with current and varyingair gap as the rotor moves. Therefore, a controller needs to be designed. For
contactless levitation, the AMB rotor requires position control in 3
independent directions(X, Y, Z).However, this control is complicated by the
mutual coupling of the 3 displacements [1], which implies design of MIMO
controller. MIMO controller implementation is very complex, and results to a
more expensive system. Instead, a decoupled control using the SISO
approach is much simpler to be improved and modified. The latter approach
is only applicable where the rotor has small deviations from its nominal
position.
Prerequisite: Modelling
Since the Magnetic Bearing is a multivariable and non linear system, we
need to linearize it and adapt it as a SISO system for easy control.
Objective
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As per request of the supervisor, the project aim is to build a digital
hardware platform able to control and stabilize ferromagnetic object in free
space, using two approaches:
The classical method and model free control
Model free control of affine chaotic systems
Sub problem 1
Design of the AMB controller using the classical method and model free
control.
Sub problem 2
Design of the same controller using the model free control of affine chaotic
systems.
Sub problem 3
Simulation using MATLAB.
Data acquisition and instrument control using LABVIEW
4. PRELIMINARY LITERATURE SURVEYMagnetic Bearings are used in various industrial applications such as
electrical power generation, petroleum refinement, machine tool operation
and natural gas handling, compressors, turbines, pumps. Magnetic bearings
are used in watt-hour meters for home power consumption. Other
applications include flywheel energy storage, artificial hearts.
Two magnetic Bearing technologies are actually used, namely:
4.1 Permanent Magnetic Bearing
This method makes use of a permanent magnet to achieve the levitation of
the rotor .No control is needed and therefore use of sensors and control
circuit is eliminated. The system is simple, but the greatest limitation is the
Earnshaws theory [3] which clearly states that group of point charges
cannot be maintained in a stable stationary equilibrium configuration solely
by the electrostatic interaction of the charges. This means that a rotor
frequently charged will be very difficult to be stabilized in free space. Thesuccess of this approach is restricted to applications where we have a small
load[4] to handle. Many researches undertaken around the world have
stated that the Permanent Magnetic bearing is physically unstable as they
are passive, and therefore a controlled active system would be more
adapted to provide better response in terms of stiffness and damping [4].
One successful experiment of this type of bearing was achieved by the NASA
Laboratory [4] for spacecraft applications in January 2008.
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4.2 Active Magnetic Bearings
While the previous approach is based on a permanent magnet, the active
magnetic bearing consists of electromagnets of which the magnetic force is
varied by the current drawn to it. Sensors, Control circuitry and power
amplifier are added to provide the necessary adjustment in case of a
deviation of the rotor from its equilibrium position. A PID controller will beused for this project. The controller will calculate the error value as the
difference between measured variable and the desired specification point to
minimize that error by adjusting the control inputs. Based on its three terms,
the PID controller can be evaluated in terms of time:(Proportional) is
implemented for the present error, I(Integral)for all past errors up to present
and D(Derivative) for predicting future errors on the systems.
A digitally controlled system makes the process much easier, especially when
it comes to modify the functionality. Analogue control systems were
restricted in that sense that any change in the system requires a hardware
change, while a digital one is software wise. A digital platform is very flexible
to adapt various types of controllers by simply changing the software.
Unfortunately, magnetic force(between the electromagnet and the rotor) is a
function changing with current and varying air gap as the rotor moves ,which
causes non linearities[5]. Non linearities are also due to the flattening of
the magnetization curve due to saturation of the core material[6], the
hysteresis of the core material depending on frequency and amplitude and
the limitations of the current and slope due to power amplifiers[6,8]. Asthe Active Magnetic bearings have high nonlinearity and instability, design of
the controller is of a great concern. Many approaches have been introduced
to control magnetic bearing system and therefore to compensate for
magnetic nonlinearities and maximize the performance of magnetic bearing
control system.
4.2.1Mathematical and Mechanical Approaches
The big challenge in that matter is to find the right force to be exerted on
the rotor .We need to estimate a simplified formula for the energy stored in
the air gap between the ferromagnetic rotor and the electromagnet core.
From there, we can derive a formula for the magnetic force.
Energy Stored in the gap
Core
Number of
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Rotor
FIGURE : ENERGY STORED IN GAP VOLUME BETWEEN THE ROTOR AND THE CORE
From electrical basics, we know that the power is determined as:
Where W is the work accomplished during a certain amount oftime t. The power where V is the voltage and I the current .Incase of an inductor, the voltage across an inductor is
L is the inductance, so its a constant. Since and we have two pole faces
present then [1]
is the permeability of air
is the spacing gap
A is the sectional area of the gap
Nis the number of turns
Partial differentiation of work over length
Keeping the current flow constant from the above formula, we can derive the
force to be exerted by electromagnets.
As the force is the derivative of the work over displacement, the magnitude
of the force will be:
AirGap
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The change in the force can be calculated as:
Lets take then we have
Where and are respectively the force/current and the force/displacement
ratios.
4.2.2 Procedures to be followed in achieving the project
Its not enough to derive a formula for the force that needs to be exerted by
the magnets in order to achieve the levitation. Many considerations are to be
taken with care, such as:
Transfer functions designs
After having the formulas for the force, the next step is to split the system in terms
of block diagrams, representing each one a specific task in the whole process. The
transfer functions to be designed are:
a. Current and gap Control loops
Because a constant control is to be done based on the gap and the current
measurements, feedback loops are required. One feedback loop will be responsible
for the air gap distance measurement and the other one consists of providing theinput to the power amplifier to produce the necessary current for the adjustment.
The air gap feedback loop will be fed to the current feedback loop.
idesired
l
Controller
2Controller
1imeasure
Controller
2Set gap
Driving
Circuit
DrivingADC ADC
Bias current
Kl Ki
Gap
Sensor
Force to be applied
Dynamics
system
response
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FIGURE : GAP AND CURRENT FEEDBACK LOOPS
[1, 10]
The force to be applied follows the rules of a simple harmonic motion (SHM) and
Newtons second law.
b. Axial Coil transfer function
This is to find the transfer function between the current to be measured and the
FIGURE : ELECTROMAGNET REPRESENTED AS A RL CIRCUIT
Voltage across the electromagnet coil, based on the Kirchhoffs voltage law,
assuming a resistor in series with an inductor.
[1]
b. Controller design
The controller design is of a great importance in order to meet the specification of
the transient response, particularly in terms of settling time. For this project, we
will decide whether a PID or a PD controller will be used. Because the system is
limited to operate at certain frequencies, there is an operating range. A controller
will also be used to attenuate frequencies beyond the stable range.
d. Sensors transfer function
Transfer function is required to scale the sensor outputs to the exact value they
represent in real life.
Simulation of the entire program
After having all the transfer functions in place, the simulation will be follow to check
whether the combined system (all the transfer functions together) responds as
expected. From this point, if the performance is after review, the simulated system
will then be implemented.
5. PROJECT SCOPE , PLANNING & COST
5.1 Project Scope
TASKS START Duration(days)
Model & transfer functions design 1/8/2013 14Controller(compensator) design 15/08/201
314
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Stability Analysis(Root locus, frequencyResponse)
29/08/2013
10
Simulation 09/09/2013
22
Prototype Implementation 1/10/2013 14Review 15/10/201
325
Final Report Compilation 9/11/2013 7review and completion of the whole project 16/11/2013
10
5.2 Gantt Chart
5.3 Project Cost
Axial Position Sensor
Type: SKF CMSS665 eddy current position sensor
Number of sensors: 5
Unit price: 3700
Cost: 18500
Power Amplifiers
Number of channels: 10
Unit Price: 4000
Number: 1
Cost: 4000
PCI Card
Type: NI PCI-6013, Low cost 200 kS/s, 16-Bit, 16-AnalogInput Multifunction DAQ
Unit price: 5910
Number: 1
Cost: 5910
6. REFERENCES
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[1]Steyn N. 2006. Digital Control System for Active Magnetic
Bearings.Tshwane University of Technology, South Africa, August
2006, page 15
[2] L. Burdet2006. Active Magnetic Bearing Design and
Characterization for High Temperature Applications.Ecole
Polytechnique Federale de la Lausanne.Switzerland,September2006,page 7
[3] A.K. PilatActive Magnetic Suspension and Bearing.AGH
University of Science and Technology ,Poland, page 2
[4] W.Morales and R. Fusaro, A. kasak. Permanent Magnetic
Bearing for Spacecraft Applications.NASA Glenn research
Center ,Cleveland,Ohio pages 5-18
[5]Jawaid I. Inayat-Hussain.Nonlinear Dynamics of aFlexible Rotorin Active Magnetic Bearings ,2007 international Symposium on
Nonlinear Theory and its Applications,Monash
University,Malaysia,pages 1-2
[6] L.Pust and O.Szollos, Interaction of two strong nonlinearities.
[7]Jianhui Zhao,Mary E.F. Kasarda,Dewey Spangler,Robert
Prins,Daniel J.Inman.Active Magnetic Bearing System
Identification using current-position perturbation
[8] L.Pust.Weak And Strong Nonlinearities In Magnetic
Bearings,Insitute of Thermomechanics ASCRDolejskova 5 18200
Prague 8,Czech Republic,February 2004
[9]Rene Larsonneur.Design and Control of Active Magnetic
Bearing Systems for High Speed Rotation.Swiss federal Institute of
Technology,Zurich,Switzerland
[10] Chip Rinaldi Sabirin, Andreas Binder, Dumitru Daniel Popa,
Aurelian Crciunescu. Modeling and Digital Control of an Active
Magnetic Bearing System