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

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International Journal of

Automatic Control System

IJACSJul–Dec 2016

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Focus and Scope of the Journal 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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A Rameshkumar Surendra Institute Of Engineering &

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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

emerging technologies.

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Automatic Control System as an emerging and increasingly vital field, now widely recognized as an integral

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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

System Analysis.

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Control System and solutions in the area.

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new developments in the field of Automatic Control System.

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editorial staff of JournalsPub, who supported us at every stage of the project.

It is our hope that this fine collection of articles will be a valuable resource for Electrical Engineering

readers and will stimulate further research into the vibrant area of Electrical Engineering.

Puneet Mehrotra

Managing Director

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 ConditionsHarjinder Singh 14

4. Response Analysis of dc Motor Using PI, PC, PD and PID ControllerDevendra Somwanshi, Gajal Parashar 20

5. Mathematical Model for Ground Electric Vehicle Using Matlab-SimulinkA. 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


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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


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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.

IJACS (2016) 20–25 © JournalsPub 2016. All Rights Reserved Page 20


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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:

IJACS (2016) 26–34 © JournalsPub 2016. All Rights Reserved Page 26


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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.

Mechanical Engineering

Chemical Engineering

Architecture

Applied Mechanics

5 more...

1 more...

2 more...2 more...

5 more...

Computer Science and Engineering

Nanotechnology« International Journal of Solid State Materials« International Journal of Optical Sciences

Physics

Civil Engineering

Electrical Engineering

Material Sciences and Engineering

Chemistry

5 more...4 more...

3 more...

Biotechnology

3 more...

Nursing « International Journal of Immunological Nursing« International Journal of Cardiovascular Nursing« International Journal of Neurological Nursing« International Journal of Orthopedic Nursing« International Journal of Oncological Nursing

5 more... 4 more...

Subm

it

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Article 2

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IJACSJul–Dec 2016

www.journalspub.com

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

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