International Journal of Automatic Control System (Vol 2 Issue 2)

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Automatic Control System
International Journal of Automatic Control System is a comprehensive journal that covers all aspects of
Automatic Control System and their integration into recent technologies that are the focus of ongoing
research. Journal has a wider scope including all major advancement in the technology and design that are
relatedtoAutomaticControlSystem.Allarticlespresentedherearepeer-reviewedandareofgood quality.
Focus and Scope oftheJournal
 Automatic Control and Systems Engineering
 Embedded Control Systems.
 Adaptive Control Techniques
 Real-Time Systems
 Real-Time and Fault-Tolerant Systems
 Large Scale Control Systems
 Intelligent Control Systems
 Stochastic Control
 Power System Control
 Perceptual Control Systems
 Digital and Analogue Control
 Motion and Navigation Control
 Temporal and Spectral System Analysis
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Dr Kaliappan E
Jaya Engineering College,
Anna University, India
Dr. Steven Sheng-Uei Guan,
Department of Computer Science & Software
Engineering, Xi'an Jiaotong-Liverpool
University, Suzhou, Jiangsu Province, China
Dr. Xiangshun Li
Wuhan University of Technology, The
University of Auckland, China
Dr. Mallikarjuna Rao Pasumarthi
Andhra university, India
Dr. V. Balaji
Bahir Dar University, Ethiopia, South Africa
Dr. D. K. Bhalla
Bhagwant Institute of Technology, Ghaziabad,
India
Dr. Vijay Raj Singh
Physics, Boston University,
United States
A Rameshkumar
Surendra Institute Of Engineering &
Management, Dhukuria, West Bengal, India
D.K. Chaturvedi
Department of Electrical Engineering, Faculty of
Engg, D.E.I., Dayalbagh, Agra, India
Mr. Saptarshi Roy
NIT Warangal, Telangana,
India
Senthil Venkatesalu,
Center For Automation Technology,
Cochin, India
Dr. Hemen Ch. Medhi,
Department of Electronics, St. Edmund's
College, Shillong,Meghalaya, India
Aseem Chandel,
B.S.A College of Engineering and Technology,
Mathura, India
Lekshmi R. R,
Department of Electrical and Electronics
Engineering, Amrita Vishwa Vidyapeetham,
Ettimadai, Coimbatore, Tamilnadu, India

From the Editor's Desk
Dear Readers,
We would like to present, with great pleasure, the inaugural volume of a new scholarly
journal, International Journal of Automatic Control System. This journal is part of the
Automatic Control System and is devoted to the scope of present Electrical Engineering
issues, from theoretical aspects to application-dependent studies and the validation of
emergingtechnologies.
This new journal was planned and established to represent the growing needs of International Journal of
Automatic Control System as an emerging and increasingly vital field, now widely recognized as an integral
part of scientific and technical investigations. Its mission is to become a voice of the Electrical Engineering
community,addressing researchersandpractitionersinthisarea.
The core vision of International Journal of Automatic Control System in JournalsPub is to propagate novel
awareness and know-how for the profit of mankind ranging from the academic and professional research
societies to industry practitioners in a range of topics in Electrical Engineering in general. Journals Pub
acts as a pathfinder for the scientific community to published their papers at excellently, well-time &
successfully.
International Journal of Automatic Control System focuses on original high-quality research in the realm of
Automatic Control System Engineering Automatic Control and Systems Engineering Embedded Control
Systems, Adaptive Control Techniques, Real-Time Systems, Real-Time and Fault-Tolerant Systems, Large
Scale Control Systems, Intelligent Control Systems, Stochastic Control, Power System Control, Perceptual
Control Systems, Digital and Analogue Control, Motion and Navigation Control, Temporal and Spectral
SystemAnalysis.
The Journal is intended as a forum for practitioners and researchers to share the techniques of Automatic
ControlSystemand solutionsinthearea.
Many scientists and researchers have contributed to the creation and the success of the Electrical
Engineering community. We are very thankful to everybody within that community who supported the idea of
creating an innovative platform. We are certain that this issue will be followed by many others, reporting
newdevelopmentsinthefieldofAutomaticControlSystem.
This issue would not have been possible without the great support of the Editorial Board members, and we
would like to express our sincere thanks to all of them. We would also like to express our gratitude to the
editorialstaffofJournalsPub,who supported us ateverystageoftheproject.
It is our hope that this fine collection of articles will be a valuable resource for Electrical Engineering
readers andwillstimulatefurtherresearchintothevibrantareaofElectricalEngineering.
PuneetMehrotra
ManagingDirector

1. Performance Analysis of Fault Tolerant Voltage Source Inverter Fed Induction Motor
Gaurav Rajoria, Garima Goswami, Ravinder Singh Chauhan 1
2. Review Insight: New Approaches for Distributed Flight Control Systems
Gagan Sarin 10
3. Experimental Investigation of Space Vector PWM-Based Matrix Converter for WECS
During Start-Up Conditions
Harjinder Singh 14
4. Response Analysis of dc Motor Using PI, PC, PD and PID Controller
Devendra Somwanshi, Gajal Parashar 20
5. Mathematical Model for Ground Electric Vehicle Using Matlab-Simulink
A. Yadav, A. Gaur, D.K. Chaturvedi 26
Contents

IJACS (2016) 1-9 © JournalsPub 2016. All Rights Reserved Page 1
International Journal of Automatic Control System
Vol. 2: Issue 2
www.journalspub.com
Performance Analysis of Fault Tolerant Voltage Source Inverter
Fed Induction Motor
Gaurav Rajoria*, Garima Goswami, Ravinder Singh Chauhan
Jaipur National University, Jaipur, India
ABSTRACT
This paper shows the execution examination of three stage induction motor fed by fault
tolerant voltage source inverter. The different fault conditions have been considered as open
leg fault, passing over one IGBT in one stage, passing over one IGBT in two distinct stages
and line to ground fault. A technique has been considered for the fault tolerant voltage
source inverter. The broken inverter leg is associated between the capacitors on the rectifier
side through controlled power switches. The system is actualized for open leg fault and the
current and THD are contrasted and ordinary voltage source inverter. The outcome
demonstrates the enhanced execution for fault tolerant voltage source inverter.
Keywords: fault analysis, fault tolerance, induction motor drive, modeling, MATLAB
simulation
INTRODUCTION
Three phase induction motors are usually
utilized as a part of mechanical
applications because of their
straightforward development, high
unwavering quality, minimal effort and so
forth. In current modern groups,
acceptance engine has been growingly
getting consideration in different ventures
including power station, car,
petrochemical, and aviation. An offbeat
engine is a kind of AC engine; the rotor
does not get electric power by conduction
but rather by the strategy for enlistment.
So these sorts of engines are called
acceptance engines.
The speed of this engine is controlled by
the recurrence of the supply current, so
these machines are generally utilized for
steady speed applications, and variable
speed renditions, utilizing variable
recurrence drives. At the point when
provided by a symmetrical and adjusted
sinusoidal three-stage voltage and working
as indicated by the producer guidelines, to
be specific to the extent the ecological
conditions and load sort are concerned, the
enlistment engine is an extremely strong
machine. Notwithstanding, deficiencies
can simply happen.
LITERATURE REVIEW
The fundamental drivers of three-stage
enlistment engine disappointments are
identified with the bearing harms and
stator flaws, especially the stator
protection breakdown in [1–3]. Presently
days the improvement of fault tolerant
enlistment engine drives has turning into a
vital research point. In view of keeping the
enlistment engine drive working even after
the event of inverter faults, a few creators
have been proposing shortcoming tolerant
working methodologies in [4–6]. This sort
of method is received to break down warm
conduct of VSI nourished acceptance
engine and figure the fault proposed to the

IJACS (2016) 10–13 © JournalsPub 2016. All Rights Reserved Page 10
Vol. 2: Issue 2
www.journalspub.com
Review Insight: New Approaches for Distributed Flight Control
Systems
Gagan Sarin*
Department of Electronics and Communication, PITS, Ujjain, India
ABSTRACT
This paper surveys the cutting edge (SOTA) in conveyed flight control advancements utilizing
openly accessible, logical and specialized distributions. Innovative improvements, for
example, installed registering and microelectromechanical frameworks are empowering
propelled aviation situated appropriated frameworks. Appropriated frameworks are
contained an extensive number of basic components, each with its own detecting, activation
and control, keeping in mind the end goal to get the wanted conduct. These frameworks can
possibly be more financial than a unified framework because of the straightforwardness of
individual parts, and plausibility of utilizing a similar generation unit for an alternate part
inside the framework. The test with these frameworks is the coordination among hubs
involving a dispersed control organizes. Advantages of conveyed design are expanded
heartiness trough excess and innate adaptation to non-critical failure. The SOTA rundown
includes a depiction of difficulties in the outline of flight control frameworks with a dispersed
structure, advances presently utilized as a part of flight control frameworks furthermore
innovations not particularly identified with appropriated flight control but rather pertinent
for the plan of future flight control methodologies. Depicted frameworks and innovations are
spoken to with cases of genuine frameworks including swarms of little Unmanned Aerial
Vehicles and dispersed systems for Fault Detection and Isolation.
Keywords: distributed control system, fault detection, isolation, SOTA
INTRODUCTION
Numerous frameworks comprise of
comparative units which straightforwardly
collaborate with their closest neighbors.
Notwithstanding when these units have
tractable models and collaborate with their
neighbors in a straightforward and
unsurprising style, the subsequent
framework frequently shows rich and
complex conduct when seen as an entirety.
There are numerous cases of such
frameworks, including computerized
roadway frameworks, plane arrangement
flight, satellite groups of stars, cross-
directional control in paper preparing
applications, and as of late, smaller scale
cantilever cluster control for enormously
parallel information capacity. One can
likewise consider lumped approximations
of halfway differential conditions (PDEs)
– cases incorporate the diversion of bars,
plates, and films, and the temperature
conveyance of thermally conductive
materials. An imperative part of a large
number of these frameworks is that
detecting what's more, incitation capacities
exist at each unit.
In the illustrations over, this is obviously
the case for mechanized thruway
frameworks, plane arrangement flight,
satellite heavenly bodies, and cross-

IJACS (2016) 14-19 © JournalsPub 2016. All Rights Reserved Page 14
Vol. 2: Issue 2
www.journalspub.com
Experimental Investigation of Space Vector PWM-Based Matrix
Converter for WECS During Start-Up Conditions
Harjinder Singh*
Department of Electrical Engineering, KC College of Engineering and Technology, Nawasher, Punjab, India
ABSTRACT
This paper displays the exploratory examination of the space vector PWM lattice converter
(MC) for wind vitality transformation framework (WECS) amid element condition. Here,
space vector PWM is successfully used to meet certain IEEE measures like IEEE 1547, IEEE-
519 and IEC 61727 principles. The control framework is actualized on a dSPACE DS1104
constant board and MATLAB/Simulink. Attainability of the proposed framework has been
tentatively confirmed utilizing a research center 1.2 kW model of WECS under startup to
unfaltering state conditions.
Keywords: matrix converter, permanent magnet synchronous generator, wind energy
conversion system (WECS), wind turbine emulator
INTRODUCTION
As of late the notoriety of a sheltered and
clean renewable vitality, especially wind
vitality has gotten and experienced
noteworthy development because of the
predictable fatigue of customary power era
strategies in view of fossil energizes,
alongside the expanding acknowledgment
of the unfavorable impacts of routine fossil
fuel control era on the earth.
Additionally, there is a blasting
advancement of silicon carbide (SiC)
based gadgets, which are significantly as
MOSFET and in addition diodes [1]. The
SiC-based gadget are additionally
encouraging later on WECS as a result of
better exchanging qualities and lower
control misfortunes as contrast with silicon
influence gadgets, however the current
influence limit of the SiC gadgets is still
insufficient for applications like wind
influence.
Because of such enormous advancement in
power semiconductor gadgets, lattice
converter have parcel of consideration by
the specialists for its application in
annoying wind control due to its high
legitimacy over conventional consecutive
voltage source converter like free from
recompense issues, enhanced voltage pick
up with streamlined control, smaller in
size, light weight, high unwavering quality
because of nonattendance of dc capacitor
and to a great degree quick transient
reaction [2–14].
Among existing generators, perpetual
magnet synchronous generators (PMSG) is
thought to be the most reasonable
generator for variable speed era since it has
particular favorable circumstances as far as
proficiency, weight, size, and unwavering
quality. It has better voltage and power
capacities. Likewise, it doesn't require
brushes and slip rings which increment the
upkeep work and cost as well.

Vol. 2: Issue 2
www.journalspub.com
Response Analysis of dc Motor Using PI, PC, PD and PID
Controller
Devendra Somwanshi, Gajal Parashar*
Poornima University Ramchandrapura, Vidhani, Sitapura, India
ABSTRACT
This paper exhibits a comparison of responses of PI-PD-PC controllers with PID controller
for a dc motor. Because of superb speed control features dc motors has been broadly utilized
in industry despites its maintenance costs are much higher than induction motor. Accordingly
speed control of dc motor has pulled in impressive research and a few techniques have
developed. The reason to control the speed of engine is to defeat the issue in industry jump at
the chance to evade machines harms and to keep away from moderate ascent time and high
overshoot. Controllers like PID controllers are utilized for the response analysis and for
control the speed of dc engine. Presently we firstly know how to simulate and modeled a dc
motor in any software and then response analysis is done through the PID controller for dc
motor. Graphical modeling in lab view software is used for the purpose of motor Modeling
and response analysis.
Keywords: dc motor, lab view, PID
INTRODUCTION
A typical actuator in control systems is the
DC motor. It straightforwardly gives
rotary motion and, combined with wheels
or drums and links, can give transitional
movement.
The electric circuit of the armature and the
free body diagram of the rotor are shown
in the following figures [1, 2].
System Equations
The motor torque, Tis identified with the
armature current, i, by a steady variable
Kt. The back emf, e, is identified with the
rotational velocity by the following
equations:
In SI units (which we will use), Kt
(armature constant) is equal to Ke (motor
constant). From the figure above we can
compose the following equations based on
Newton's law combined with Kirchhoff's
law:

Vol. 2: Issue 2
www.journalspub.com
Mathematical Model for Ground Electric Vehicle Using Matlab-
Simulink
A. Yadav*, A. Gaur, D.K. Chaturvedi
Department of Electrical Engineering,DEI,Dayalbagh, Agra, India
ABSTRACT
Mathematical modeling of electric vehicle is present in this work. This mathematical
modeling gives fast response, accuracy and it show all the function of moving electric
vehicle. Also describes the application of MATLAB modeling and simulation. A method is
described to extract the model parameters and to approximate estimation of the internal
system. The model is validated superimposing the results with the design discharge curves.
Finally, the battery model is included in the SimPowerSystem simulation software and is
used in the Electric Vehicle (EV) demo. A simplified mathematical model for ground electric
vehicle is developed as per the objective. For making the full simulation environment, the
control law would also be developed in Simulink and testing would be carried out finally the
control law would be translated in software for intended hardware and real EV will be
achieved. Modelling and simulation of systems by using various parameters, software will
facilitate the process of designing, constructing and inspecting the vehicle in the real world.
One can investigate, design, visualize, and test an object or even if it does not exists
Keywords: individual difference, mathematical model, model interfacing, speed control
INTRODUCTION
The future technologies related to electric
vehicles (EV) are the most important
alternatives to cope with the reduction of
greenhouse gases. In particular, plug-in
EV and vehicle-to-grid concepts will have
a tremendous effect not only on the
reduction of the greenhouse gases but also
on the electricity distribution systems.
Above all, these new technique will
heavily depend on the battery system. It is
therefore important to design and develop
accurate electric battery models that can
easily use with the simulators of power
systems and on-board power electronic
systems. In this paper, a system using only
state of charge as a state variable chosen
in order to accurately reproduce the
manufacturer’s curves for the battery
chemistries. The paper is categorised into
three sections. In the first section, the
proposed system model and its parameters
are described. In addition, a methodology
presented to show how to determine the
model parameters from the developers
discharge curves of battery. In the second
section, the discharge curves are obtained
by modelling and simulation with the
designed datasheets. The third section
contains the example of an application
where the battery model integrated to the
Sim Power Systems is used in the
complete simulation of an EV power
system.
THE BATTERY MODEL
The battery is using a simple voltage
controlled source in series with a constant
resistance, as shown in Figure. This model
assumes the same features for the charge
the discharge cycles. The open voltage
source is calculated by non-linear equation
based on the actual SOC of the battery.

International Journal of Automatic Control System (Vol 2 Issue 2)

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