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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 559
SPEED CONTROL OF INDUCTION MOTOR USING HYSTERESIS METHOD
Vidhya Krishnan G1, C.Hemalatha 2
1 Assistant Professor, Electrical & Electronics Engineering, Gnanamani College of Technology, TamilNadu, India
2 Assistant Professor, Electrical & Electronics Engineering, Gnanamani College of Technology, TamilNadu, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - The speed-regulation problem for induction
motor system is studied in this Project. In order to
optimize the control performance of the IM, the
hysteresis current control method is introduced in the
control design of speed loop. In the system predictive
voltage controller based on speed of the induction
motor by the observer is implemented A simplified
model is employed to predict the future speed of IM.
Then, an optimal control law is obtained by minimizing
a quadratic performance index. However, it is noted
that the standard current control method does not
achieve a satisfying effect in the presence of strong
disturbances. To this end, an improved hysteresis
method is developed. It introduces extended state
observer (ESO) to estimate the lumped disturbances
and adds a feed forward compensation item based on
the estimated disturbances to the speed controller. The
stator current can be easily adjusted by modulating the
pulse width of the switching device during the
alignment. Some experiments are implemented on a
single chip ARM processor to demonstrate the
feasibility of the sensor less and start up techniques.
Key Words: Hysteresis Method, Speed regulation,
Induction Motor, Controller, ARM processor
1. INTRODUCTION
One of the mature control systems of induction motor is
the field oriented control method. The FOC method is
widely used and presents some high standards in modern
industrial drives. A continuous trend in IM drives is to
increase the reliability of the drive system. One solution is
to decrease the amount of normally used sensors. Because
of noises and other disadvantages the troublesome device
in some of industrial drive system is the speed sensor.
Therefore, in most modern IM drives speed sensor
elimination is required. Instead of a speed sensor,
different methods for speed calculation are proposed in
the literature. Comprehensive reviews of the IM sensor
less drives are given, indicating that some problems with
the sensor less control are persistent, so new solutions are
still needed. Current work efforts are dedicated
particularly to zero or very low speed range or to very
high performance drives. Another problem in electrical
drives is system sensitivity to inaccuracy and changes of
motor equivalent circuit parameters. Most of the FOC
systems are very sensitive to that inaccuracy so some
parameters should be estimated on-line. Also, robust
structures of the control and estimation schemes are
generally researched.
2. INDUCTION MOTOR
Like any electric motor, a 3-phase induction motor has a
stator and a rotor. The stator carries a 3-phasewinding
(called stator winding) while the rotor carries a short-
circuited winding(called rotor winding).Only the stator
winding is fed from 3-phase supply. The rotor winding
derives its voltage and power from the externally
energized stator winding through electromagnetic
induction and hence the name. The induction motor may
be considered to be a transformer with a rotating
secondary and it can, therefore, be described as a
“transformer- type” a.c. machine in which electrical
energy is converted into mechanical energy.
A 3-phase induction motor has two main parts (i)stator
and(ii)rotor. The rotor is separated from the stator by a
small air-gap which ranges from 0.4mm to 4 mm,
depending on the power of the motor.
2.1 Stator
The insulated connected to form a balanced 3-phase star or
delta connected circuit. The 3-phase stator winding is
wound for a definite number of poles as per requirement of
speed. Greater the number of poles, lesser is the speed of
the motor and vice-versa. When 3-phase supply is given to
the stator winding, a rotating magnetic field of constant
magnitude is produced. This rotating field induces currents
in the rotor by electromagnetic induction.
It consists of a steel frame encloses a hollow
cylindrical core made up of thin laminations of silicon steel
to reduce the hysteresis and eddy current losses.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 560
2.2 Rotor
The rotor mounted on a shaft, is a hollow laminated core
having slots on its outer periphery. The winding placed in
these slots (called rotor winding) may be one of the
following two types:
(i) Squirrel cage type
(ii) Wound type
Squirrel cage rotor. It consists of a laminated cylindrical
core having parallel slots on its outer periphery. One
copper or aluminum bar is placed in each slot. All these
bars are joined at each end by metal rings called end ring.
This forms a permanently short-circuited winding which is
indestructible. The entire construction (bars and end
rings) resembles a squirrel cage and hence the name. The
rotor is not connected electrically to the supply but has
current induced in it by transformer action from the stator.
Those induction motors which employ squirrel cage rotor
are called squirrel cage induction motors. Most of 3-phase
induction motors use squirrel cage rotor as it has a
remarkably simple and robust construction enabling it to
operate in the most adverse circumstances. However, it
suffers from the disadvantage of a low starting torque. It is
because the rotor bars are permanently short-circuited
and it is not possible to add any external resistance to the
rotor circuit to have a large starting torque.
Fig -1: Rotor Windings
Wound rotor. It consists of a laminated cylindrical core
and carries a 3- phase winding, similar to the one on the
stator .The rotor winding is uniformly distributed in the
slots and is usually star-connected. The open ends of the
rotor winding are brought out and joined to three
insulated slip rings mounted on the rotor shaft with one
brush resting on each slip ring. The three brushes are
connected to a 3-phase star-connected rheostat. At
starting, the external resistances are included in the rotor
circuit to give a large starting torque. These resistances
are gradually reduced to zero as the motor runs up to
speed.
Fig -2: Rotor Windings
3. INVERTER
The converter chops the input DC voltage and generates
an AC voltage with desired magnitude and frequency with
respect to the pulse patterns and modulation techniques.
Different current and voltage control methods have been
proposed to generate a high voltage high current
rectangular waveform based on reference voltage
characteristics.
3.1 Diode-Clamped Inverter
The diode-clamped inverter, also called neutral-point
clamped (NPC) inverter, is the most common type of
converter used for distributed generation such as wind
turbine and photovoltaic.
The principle of diode clamping to DC link voltages can be
extended to any number of voltage levels.. Since the
voltage across the semiconductor switches are limited by
conduction of the diodes connected to the various DC
levels, this class of multi level inverters is termed diode
clamped multi level inverters. For the case a three-level
diode-clamped inverter is shown in Figure. It consists of
two pairs of switches and two diodes.
Each switch pairs works in complimentary mode and the
diodes are used to provide access to mid-point voltage.
The DC bus voltage is split into three voltage levels by
using two series connection of DC capacitors, C1 and C2.
Each capacitor is supposed to have an equal DC voltage
and each voltage stress will be limited to one capacitor
level through clamping diodes (Dc1 and Dc2). If assumed
that total DC link voltage is Vdc and mid point is regulated
at half of the DC link voltage, the voltage across each
capacitor is Vdc/2 (Vc1=Vc2=Vdc/2). Based on the
structure of the diode-clamped converter, there are three
different possible switching states which apply the
staircase voltage on output voltage relating to DC link
capacitor voltage rate. To study the effect of the number of
output voltage levels in diode-clamped topology, If
converter works in balance condition, DC link voltage is
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 561
split in three equal values by the series capacitors
(Vc1=Vc2=Vc3=Vdc/3).
Fig -3: (a) Three-level and (b) Four-level diode
clamped Inverter
Advantages
 Harmonic content is low
 Filter is not necessary
 High efficiency
3.2 Flying-Capacitor Multilevel Inverter
A multi-cell or a flying-capacitor multilevel inverter
(FCMI) does not require isolated DC sides and additional
clamping diodes; snubber-less operation is possible and
expansion to multilevel is easy. However, these properties
may be limited by voltage unbalancing of flying capacitors,
which is the most serious problem. Therefore, the FCMI
has to ensure voltage balancing of the flying capacitors,
under all operating conditions.
This configuration is an alternative to the diode-clamped
converter, however, voltage across an open switch is
constrained by clamping capacitors instead of clamping
diode in diode-clamped topology. Therefore, it can avoid
the use of multiple diodes at the higher voltage levels.
Although this type of converter shares the advantages of
all multilevel inverters, it faces with some problems.
One of the main problems is the requirement of
complicated control strategy due to regulation of floating
capacitor voltages another problem is associated with
converter initialization that means before the flying
capacitor inverter can be modulated, the clamping
capacitors must be setup with the required voltage level.
By increasing the number of levels, more capacitors are
needed. If the input DC link is Vdc and the flying capacitor
works in balance condition mode, in order to have an
equal step voltages at output voltage, clamped capacitor
should regulated at Vc1=Vdc/2 in the three-level inverter
and Vc2= 2Vc1=2Vdc/3 in the four-level inverter. It is note
that along with increasing the output voltage quality in
four-level structure, voltage stress on switching
components reduces by Vdc/6.
Fig -4: (a)Three-level and (b) Four-level Flying
capacitor Inverter
Advantages
 Phase Redundancies are available for balancing the
voltage levels of the capacitors.
 Real and reactive power flow can be controlled.
 The large number of capacitors enables the inverter
to ride through short duration outages and deep voltage
sags.
3.2 Cascade Multilevel Inverter
A cascade multilevel inverter is made up of a series of H-
bridge (single-phase full-bridge) inverters, each with their
own isolated dc-bus. The multilevel inverter can generate
almost- sinusoidal waveform voltage from several
Separate DC Sources (SDCSs), which may be obtained from
solar cells, fuel cells, batteries, ultra capacitors etc.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 562
The third topology for a multilevel converter is
the cascade inverter, which can be synthesised by a series
of single-phase full-bridge inverters. Assuming that the DC
voltage of each full-bridge cell is same and equal to Vdc/2,
each full-bridge inverter can switch between –Vdc,/2,0,
and Vdc,/2. Therefore, by adding and subtracting of the
output voltage levels of the two cascaded full-bridge
inverter cells, five different voltage levels can be achieved
in the output voltage. Switching states associated with
different output voltage levels for the cascade inverter
with two full-bridge inverter cells. Three-phase
configuration can be easily implemented by three single-
phase structures. Cascade configuration has been
attracted for medium and high voltage renewable energy
systems such as photovoltaic, due to its modular and
simple structure. A higher level can easily be implemented
by adding classical H-bridge cells in this configuration.
However, it needs additional DC voltage sources and
switching devices which can increase the cost of the
system.
Fig -5: (a) Five –level and (b) Seven-level cascade Inverter
Advantages
 Its active devices switching at (or nearly) the
fundamental frequency, drastically reducing switching
losses.
 Elimination of the transformer in providing
required voltage levels.
 Easier packaging due to the simplicity of its
structure and its low component-count.
5.HYSTERESIS METHOD
Fig -6: Block Diagram
RECTIFIER INVERTER
ARM
CONTROLLER
PULSE
WIDTH
MODULATO
R
MOT
OR
C
T
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 563
5.1 Simulation Diagram
Fig -7: Simulation Diagram
6. RESULT
The result were satisfactory and up to the expected level.
This paper aims at intending an effective method to
control the speed of the induction motor by using
hysteresis method. The output can be obtained by using
system interfaces and also dock light software is used to
display the output. The output will be the frequency and
time period. The speed can be changed step by step
according to input sequence. The speed of the motor can
be varied from 600 rpm to 1000 rpm.
7. CONCLUSION AND FUTURE WORK
To control the speed of a 3-phase induction motor in open
loop, supply voltage and frequency need to be varied with
constant ratio to each other. A low cost solution of this
control can be implemented in ARM Processor. This
requires three PWMs to control a 3-phase inverter bridge.
Many ARM Processors have two hardware PWMs. The
third PWM is generated in software and output to a port
pin. Speed range of motor is 600 rpm to 1000 rpm.
The induction motor is run at 1000rpm to 600rpm.In
future it will run at above 1000rpm by increasing the
number of sequences.
8. REFERENCES
[1] J. Shao,” An improved microprocessor based sensor
less brushless DC (BLDC) motor drive for automotive
applications, ”IEEETrans.Ind.Appl.,Vol.42,no.5,pp.1216-
1221,sep/oct 2010.
[2] J. Fang ,X. Zhou and G. Liu ,”Instantaneous torque
control of small inductance brushless DC motor.” IEEE
transactions.PowerElectron,vol.28,no.3,pp.1400-1412,Mar
2013.
[3] J. Fang, X. Zhou, and G. Liu, “Instantaneous torque
control of small inductance brushless DC motor,” IEEE
Trans. Power Electron., vol.27, no.12, pp.4952-4964, Dec.
2012.
[4] J. Su and J. W. Mc Keever, “Low-cost sensor less
control of brushless DC motors with improved speed
range,” IEEE Trans. Power Electron., vol.19, no.2, pp.296-
302, Mar. 2004.
[5] D. H. Jung and I. J. Ha, “Low-cost sensor less control of
brushless DC motors using a frequency-independent
phase shifter,” IEEE Trans. Power Electron., vol.15, no.4,
pp.744-752, July, 2000.
[6] R. C. Becerra, T. M. Jahns, and M. Ehsani, “Four-
quadrant sensorless brushless ECM drive,” in Proc. IEEE-
APEC’91 Conf., 1991, pp.202-209.
[7] T. M. Jahn, R. C. Becerra, and M. Ehsani, “Integrated
current regulation for a brushless ECM drive,” IEEE
Trans. Power Electron., vol.6, no.1, pp.118-126, Jan. 1991.
[8] I. Takahashi and T. Noguchi, “A new quick-response
and high-efficiency control

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Speed Control of Induction Motor Using Hysteresis Method

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 559 SPEED CONTROL OF INDUCTION MOTOR USING HYSTERESIS METHOD Vidhya Krishnan G1, C.Hemalatha 2 1 Assistant Professor, Electrical & Electronics Engineering, Gnanamani College of Technology, TamilNadu, India 2 Assistant Professor, Electrical & Electronics Engineering, Gnanamani College of Technology, TamilNadu, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - The speed-regulation problem for induction motor system is studied in this Project. In order to optimize the control performance of the IM, the hysteresis current control method is introduced in the control design of speed loop. In the system predictive voltage controller based on speed of the induction motor by the observer is implemented A simplified model is employed to predict the future speed of IM. Then, an optimal control law is obtained by minimizing a quadratic performance index. However, it is noted that the standard current control method does not achieve a satisfying effect in the presence of strong disturbances. To this end, an improved hysteresis method is developed. It introduces extended state observer (ESO) to estimate the lumped disturbances and adds a feed forward compensation item based on the estimated disturbances to the speed controller. The stator current can be easily adjusted by modulating the pulse width of the switching device during the alignment. Some experiments are implemented on a single chip ARM processor to demonstrate the feasibility of the sensor less and start up techniques. Key Words: Hysteresis Method, Speed regulation, Induction Motor, Controller, ARM processor 1. INTRODUCTION One of the mature control systems of induction motor is the field oriented control method. The FOC method is widely used and presents some high standards in modern industrial drives. A continuous trend in IM drives is to increase the reliability of the drive system. One solution is to decrease the amount of normally used sensors. Because of noises and other disadvantages the troublesome device in some of industrial drive system is the speed sensor. Therefore, in most modern IM drives speed sensor elimination is required. Instead of a speed sensor, different methods for speed calculation are proposed in the literature. Comprehensive reviews of the IM sensor less drives are given, indicating that some problems with the sensor less control are persistent, so new solutions are still needed. Current work efforts are dedicated particularly to zero or very low speed range or to very high performance drives. Another problem in electrical drives is system sensitivity to inaccuracy and changes of motor equivalent circuit parameters. Most of the FOC systems are very sensitive to that inaccuracy so some parameters should be estimated on-line. Also, robust structures of the control and estimation schemes are generally researched. 2. INDUCTION MOTOR Like any electric motor, a 3-phase induction motor has a stator and a rotor. The stator carries a 3-phasewinding (called stator winding) while the rotor carries a short- circuited winding(called rotor winding).Only the stator winding is fed from 3-phase supply. The rotor winding derives its voltage and power from the externally energized stator winding through electromagnetic induction and hence the name. The induction motor may be considered to be a transformer with a rotating secondary and it can, therefore, be described as a “transformer- type” a.c. machine in which electrical energy is converted into mechanical energy. A 3-phase induction motor has two main parts (i)stator and(ii)rotor. The rotor is separated from the stator by a small air-gap which ranges from 0.4mm to 4 mm, depending on the power of the motor. 2.1 Stator The insulated connected to form a balanced 3-phase star or delta connected circuit. The 3-phase stator winding is wound for a definite number of poles as per requirement of speed. Greater the number of poles, lesser is the speed of the motor and vice-versa. When 3-phase supply is given to the stator winding, a rotating magnetic field of constant magnitude is produced. This rotating field induces currents in the rotor by electromagnetic induction. It consists of a steel frame encloses a hollow cylindrical core made up of thin laminations of silicon steel to reduce the hysteresis and eddy current losses.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 560 2.2 Rotor The rotor mounted on a shaft, is a hollow laminated core having slots on its outer periphery. The winding placed in these slots (called rotor winding) may be one of the following two types: (i) Squirrel cage type (ii) Wound type Squirrel cage rotor. It consists of a laminated cylindrical core having parallel slots on its outer periphery. One copper or aluminum bar is placed in each slot. All these bars are joined at each end by metal rings called end ring. This forms a permanently short-circuited winding which is indestructible. The entire construction (bars and end rings) resembles a squirrel cage and hence the name. The rotor is not connected electrically to the supply but has current induced in it by transformer action from the stator. Those induction motors which employ squirrel cage rotor are called squirrel cage induction motors. Most of 3-phase induction motors use squirrel cage rotor as it has a remarkably simple and robust construction enabling it to operate in the most adverse circumstances. However, it suffers from the disadvantage of a low starting torque. It is because the rotor bars are permanently short-circuited and it is not possible to add any external resistance to the rotor circuit to have a large starting torque. Fig -1: Rotor Windings Wound rotor. It consists of a laminated cylindrical core and carries a 3- phase winding, similar to the one on the stator .The rotor winding is uniformly distributed in the slots and is usually star-connected. The open ends of the rotor winding are brought out and joined to three insulated slip rings mounted on the rotor shaft with one brush resting on each slip ring. The three brushes are connected to a 3-phase star-connected rheostat. At starting, the external resistances are included in the rotor circuit to give a large starting torque. These resistances are gradually reduced to zero as the motor runs up to speed. Fig -2: Rotor Windings 3. INVERTER The converter chops the input DC voltage and generates an AC voltage with desired magnitude and frequency with respect to the pulse patterns and modulation techniques. Different current and voltage control methods have been proposed to generate a high voltage high current rectangular waveform based on reference voltage characteristics. 3.1 Diode-Clamped Inverter The diode-clamped inverter, also called neutral-point clamped (NPC) inverter, is the most common type of converter used for distributed generation such as wind turbine and photovoltaic. The principle of diode clamping to DC link voltages can be extended to any number of voltage levels.. Since the voltage across the semiconductor switches are limited by conduction of the diodes connected to the various DC levels, this class of multi level inverters is termed diode clamped multi level inverters. For the case a three-level diode-clamped inverter is shown in Figure. It consists of two pairs of switches and two diodes. Each switch pairs works in complimentary mode and the diodes are used to provide access to mid-point voltage. The DC bus voltage is split into three voltage levels by using two series connection of DC capacitors, C1 and C2. Each capacitor is supposed to have an equal DC voltage and each voltage stress will be limited to one capacitor level through clamping diodes (Dc1 and Dc2). If assumed that total DC link voltage is Vdc and mid point is regulated at half of the DC link voltage, the voltage across each capacitor is Vdc/2 (Vc1=Vc2=Vdc/2). Based on the structure of the diode-clamped converter, there are three different possible switching states which apply the staircase voltage on output voltage relating to DC link capacitor voltage rate. To study the effect of the number of output voltage levels in diode-clamped topology, If converter works in balance condition, DC link voltage is
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 561 split in three equal values by the series capacitors (Vc1=Vc2=Vc3=Vdc/3). Fig -3: (a) Three-level and (b) Four-level diode clamped Inverter Advantages  Harmonic content is low  Filter is not necessary  High efficiency 3.2 Flying-Capacitor Multilevel Inverter A multi-cell or a flying-capacitor multilevel inverter (FCMI) does not require isolated DC sides and additional clamping diodes; snubber-less operation is possible and expansion to multilevel is easy. However, these properties may be limited by voltage unbalancing of flying capacitors, which is the most serious problem. Therefore, the FCMI has to ensure voltage balancing of the flying capacitors, under all operating conditions. This configuration is an alternative to the diode-clamped converter, however, voltage across an open switch is constrained by clamping capacitors instead of clamping diode in diode-clamped topology. Therefore, it can avoid the use of multiple diodes at the higher voltage levels. Although this type of converter shares the advantages of all multilevel inverters, it faces with some problems. One of the main problems is the requirement of complicated control strategy due to regulation of floating capacitor voltages another problem is associated with converter initialization that means before the flying capacitor inverter can be modulated, the clamping capacitors must be setup with the required voltage level. By increasing the number of levels, more capacitors are needed. If the input DC link is Vdc and the flying capacitor works in balance condition mode, in order to have an equal step voltages at output voltage, clamped capacitor should regulated at Vc1=Vdc/2 in the three-level inverter and Vc2= 2Vc1=2Vdc/3 in the four-level inverter. It is note that along with increasing the output voltage quality in four-level structure, voltage stress on switching components reduces by Vdc/6. Fig -4: (a)Three-level and (b) Four-level Flying capacitor Inverter Advantages  Phase Redundancies are available for balancing the voltage levels of the capacitors.  Real and reactive power flow can be controlled.  The large number of capacitors enables the inverter to ride through short duration outages and deep voltage sags. 3.2 Cascade Multilevel Inverter A cascade multilevel inverter is made up of a series of H- bridge (single-phase full-bridge) inverters, each with their own isolated dc-bus. The multilevel inverter can generate almost- sinusoidal waveform voltage from several Separate DC Sources (SDCSs), which may be obtained from solar cells, fuel cells, batteries, ultra capacitors etc.
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 562 The third topology for a multilevel converter is the cascade inverter, which can be synthesised by a series of single-phase full-bridge inverters. Assuming that the DC voltage of each full-bridge cell is same and equal to Vdc/2, each full-bridge inverter can switch between –Vdc,/2,0, and Vdc,/2. Therefore, by adding and subtracting of the output voltage levels of the two cascaded full-bridge inverter cells, five different voltage levels can be achieved in the output voltage. Switching states associated with different output voltage levels for the cascade inverter with two full-bridge inverter cells. Three-phase configuration can be easily implemented by three single- phase structures. Cascade configuration has been attracted for medium and high voltage renewable energy systems such as photovoltaic, due to its modular and simple structure. A higher level can easily be implemented by adding classical H-bridge cells in this configuration. However, it needs additional DC voltage sources and switching devices which can increase the cost of the system. Fig -5: (a) Five –level and (b) Seven-level cascade Inverter Advantages  Its active devices switching at (or nearly) the fundamental frequency, drastically reducing switching losses.  Elimination of the transformer in providing required voltage levels.  Easier packaging due to the simplicity of its structure and its low component-count. 5.HYSTERESIS METHOD Fig -6: Block Diagram RECTIFIER INVERTER ARM CONTROLLER PULSE WIDTH MODULATO R MOT OR C T
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 01 | Jan-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 563 5.1 Simulation Diagram Fig -7: Simulation Diagram 6. RESULT The result were satisfactory and up to the expected level. This paper aims at intending an effective method to control the speed of the induction motor by using hysteresis method. The output can be obtained by using system interfaces and also dock light software is used to display the output. The output will be the frequency and time period. The speed can be changed step by step according to input sequence. The speed of the motor can be varied from 600 rpm to 1000 rpm. 7. CONCLUSION AND FUTURE WORK To control the speed of a 3-phase induction motor in open loop, supply voltage and frequency need to be varied with constant ratio to each other. A low cost solution of this control can be implemented in ARM Processor. This requires three PWMs to control a 3-phase inverter bridge. Many ARM Processors have two hardware PWMs. The third PWM is generated in software and output to a port pin. Speed range of motor is 600 rpm to 1000 rpm. The induction motor is run at 1000rpm to 600rpm.In future it will run at above 1000rpm by increasing the number of sequences. 8. REFERENCES [1] J. Shao,” An improved microprocessor based sensor less brushless DC (BLDC) motor drive for automotive applications, ”IEEETrans.Ind.Appl.,Vol.42,no.5,pp.1216- 1221,sep/oct 2010. [2] J. Fang ,X. Zhou and G. Liu ,”Instantaneous torque control of small inductance brushless DC motor.” IEEE transactions.PowerElectron,vol.28,no.3,pp.1400-1412,Mar 2013. [3] J. Fang, X. Zhou, and G. Liu, “Instantaneous torque control of small inductance brushless DC motor,” IEEE Trans. Power Electron., vol.27, no.12, pp.4952-4964, Dec. 2012. [4] J. Su and J. W. Mc Keever, “Low-cost sensor less control of brushless DC motors with improved speed range,” IEEE Trans. Power Electron., vol.19, no.2, pp.296- 302, Mar. 2004. [5] D. H. Jung and I. J. Ha, “Low-cost sensor less control of brushless DC motors using a frequency-independent phase shifter,” IEEE Trans. Power Electron., vol.15, no.4, pp.744-752, July, 2000. [6] R. C. Becerra, T. M. Jahns, and M. Ehsani, “Four- quadrant sensorless brushless ECM drive,” in Proc. IEEE- APEC’91 Conf., 1991, pp.202-209. [7] T. M. Jahn, R. C. Becerra, and M. Ehsani, “Integrated current regulation for a brushless ECM drive,” IEEE Trans. Power Electron., vol.6, no.1, pp.118-126, Jan. 1991. [8] I. Takahashi and T. Noguchi, “A new quick-response and high-efficiency control