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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

    .......................................................... .................................

    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

    ......................................................... ................................

    SIGNATURE DATE

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    DETAILS OF MODERATOR

    SURNAME AND INITIALS:.................................................................................

    INSTITUTE: ..........................................................................................................

    QUALIFICATION: ...................................................................................................

    TELEPHONE NUMBER: ........................................................................................

    FAX NUMBER: ...................................................................................................

    ......................................................... ................................

    SIGNATURE DATE

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    DETAILS OF REPRESENTATIVE

    SURNAME AND INITIALS: .................................................................................

    INSTITUTE: .........................................................................................................

    QUALIFICATION: ..................................................................................................

    TELEPHONE NUMBER: .......................................................................................

    FAX NUMBER: ..................................................................................................

    ......................................................... ................................

    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