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IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 210
STEADY STATE STABILITY ANALYSIS AND ENHANCEMENT OF
THREE MACHINE NINE BUS POWER SYSTEM USING TCPS FACTS
DEVICE
Divya Rishi Shrivastava1
, Daneshwari R Akkishetti 2
1
Assistant Professor, Electrical & Electronics Dept., Manipal University Jaipur, Rajasthan, India
2
Lecturer, Electrical & Electronics Dept., Jain College of Engineering Belgaum, Karnataka, India
Abstract
Power System stability study is the important parameter of economic, reliable and secure system planning and operation. Studies
are important during the planning and conceptual design stages of the project as well as during the operating life of the plant
periodically. This paper presents the power system steady state stability analysis for IEEE- 9 bus test system and examines
influence of TCPS FACTS device based controller on test system. It is assumed that system under study has been perturbed from a
steady state equilibrium that prevailed prior to the application of the disturbance. If system is stable, we would expect that for
temporary or permanent disturbance, system will acquire initial or new operating state after a transient period. The stability
study is accessed using Lyapunov’s first method. The effectiveness of damping controller in enhancing the steady state stability is
investigated by incorporating available constraints. For analysis MATLAB software is employed. The conclusions have been
drawn here, based on theoretical and mathematical analysis so as to provide an insight and better understanding of steady state
stability of considered multi machine power system.
Key Words: Lyapunov’s first method, Steady-state stability, Phase portrait, FACTS device, supplementary modulation
controller, eigen value, synchronizing power coefficient, IEEE-9 Bus Test System, Load Flow Study, Differential
algebraic equation.
--------------------------------------------------------------------***----------------------------------------------------------------------
1. INTRODUCTION
Power system stability may be defined as property of a
power system that enables it to remain in a state of operating
equilibrium under normal operating conditions and to regain
an acceptable state of equilibrium after being subjected to a
disturbance [4]. The oscillations, which are typically in the
frequency range of 0.2 to 3.0 Hz, might be excited by the
disturbances in the system [1][13] or, in some cases, might
even build up spontaneously. A power system at a given
operating condition may be unstable due to large
disturbance; still such a system can be operated, though
insecurely. However, if the system is small signal unstable
at a given operating condition, it cannot be operated.
Therefore, steady state stability is a fundamental
requirement for satisfactory operation of power system.
Instability that may result can be of two forms i)increase in
rotor angle through a non-oscillatory or aperiodic mode due
to lack of synchronizing torque, or ii)rotor oscillation of
increasing amplitude due to lack of sufficient damping
torque[13].With the advent of FACTS devices, and due to
recent advances in power electronics , its capability to
enhance oscillation damping and system stability has been
explored as potential application. With advent of high
power, high speed electronic FACTS controllers have been
mainly used for solving various power system control
problems such as voltage regulation, power flow, and
transfer capability enhancement. As supplementary
functions, they have been in use for damping the inter area
modes and enhancing power system stability [3].
This paper studies theoretical and mathematical analysis of
IEEE 3- machine – 9 bus power system and the influence of
the TCPS FACTS device based controller on the steady state
stability about an operating condition. Here, controller
parameters are obtained by incorporating available
constraints. The Mathematical analysis is carried out in
MATLAB using eigenvalue analysis, phase portrait and
time domain analysis of state variable of power system
when subjected to small disturbance.
1.1 IEEE -3 Machine 9 Bus Power System
We have considered the popular Western System
Coordinated Council (WSSC), IEEE 3-machine, 9-bus
system shown in fig.1. This system is also appearing in
references [8] and [10].The base MVA is 100 and system
frequency is 60Hz. The system data are given in Appendix I.
Classical model of the generators are employed for analysis.
The operating conditions are obtained by using Load flow
analysis. Eigen value analysis and phase portrait for
concerned state variable are drawn about available operating
state. The Enhancement in steady state stability is analyzed
by incorporating TCPS FACTS device based controller, the
gains of which are taken by incorporating available
constraints. For Analysis TCPS FACTS device is placed
between Machine 1 and 2.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 211
1.2 Mathematical Model
A load flow study of a power system shown in Fig. 1, is
done to determine electrical power output of machine i and
to calculate values of for all generators.
Fig-1 IEEE 3-machine 9-bus power system
The power into the network at node i,
(1)
Where,
= negative of the transfer admittance between nodes i and j.
= driving point admittance for node i.
Once Y matrix is calculated, we eliminate all the nodes
expect for the internal generator nodes and obtain the Y
matrix for reduced network. The reduction can be achieved
by matrix operation considering fact that all the nodes have
zero injection currents except for the internal generator
nodes. In a power system with n generators, the nodal
equation can be written as,
(2)
Where subscript n is used to denote generator nodes and
subscript r is used for the remaining nodes.
Expanding Eq. (2)
0=
From which we eliminate to find
)
) (3)
It has dimensions ( where n is the number of
generators. This convenient analytic technique that can be
used only when the loads are treated as constant impedance
[8][11]. The equation of motion for i th machine given by,
+
(4)
(5)
The electrical power is given by Eq.(1). Linearizing
Eq.(1) and (5) about initial operating condition [4]
represented by = yields,
(6)
defined as synchronizing power coefficient [4].
The test power system is now linearized about initial
operating condition available from load flow. The classical
model [6][7]of a synchronous machine is used to study the
stability of a power system. Linearizing multi machine
system about an initial operating condition using equations
(4) and (5) gives,
(7)
When generator 2 and 3 are swinging with respect to
generator 1,
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 212
(8)
From Eq. (8) the state space representation of the test system
is given by,
21 21
21 21 23 21 1
1
31 31
31 41 43 31 1
2
2 3
3
0 1 0 0 0
0 0 / 2
0 0 0 1 0
0 0 / 2
0 0
/ 2 0
0 / 2
0 0
r
r
r
r
A A w Hd
Pm
dt
A A w H
w H
Pm Pm
w H
 
 
 
 
        
                   
        
       
        
   
   
     
   
   
   
(9)
Where Eq. are formed using Eq. (8). Eq. (9) is written in
standard control theory form , where
X is state variable vector and U is the control variable
vector. Applying controllability criterion to all three input
matrix,
It should follow,
C=n [1 : 1 : 1]
Where n is size of Jacobian matrix.
2.TCPS FACTS DEVICE BASED CONTROLLER
MODELLING
Thyristor controlled phase shifter is used to enhance steady
state stability of power system. TCPS FACTS device based
controller enable fast control of the phase angle ( and it is
determined as non linear function of rotor angle and speed.
It is used to damp low frequency oscillation. For TCPS
FACTS device based damping controller generally
Supplementary Modulation Controller are recommended
[2],by designing a SMC for the damping controller based on
rotor speed signal as input, it is possible to enhance the
damping and stabilize swing mode. TCPS FACTS device
based controllers are based on conventional lead-lag type.
Here and provide the required phase compensation to
give necessary damping. is washout circuit time constant,
wash out circuit serves as a high pass filter with time
constant varies from 10s to 20s [2].
Fig-2 Structure of TCPS based controller
Controllable parameter of the TCPS FACTS device based
controller is that is rotor angle of generator and the control
law is,
The transfer function of controller is given by,
(10)
Differential algebraic equation of damping controller can be
formulated from Eq.(10)
(11)
Here, controller parameters are obtained by incorporating
available constraints such as,
i) No new mode of oscillation should evolve
ii) Damping in the system that should be,0< ζ ≤ 1
iii) All states variables should be controllable
2.1 Mathematical Modelling IEEE 9 Bus Power
System with TCPS Facts Device
Fig-3 Reduced figure 1 with damping controller
The test power system is equipped with TCPS FACTS
device based controller near generator terminal between bus
2 and 1 as shown in Fig.3. As losses of the thyristors are a
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 213
small proportion of the DC link power and quadrature power
inserted by transformer is small proportion of the line
primary power so that phase shifter losses are neglected [12]
and Time constant of thyristors is very short; and can be
neglected for computation [12]. The dynamic equation of
system with damping controller are obtained by Eq. (8) and
(11), linearizing these equations about operating point we
get,
(12)
The state space representation of test system with damping
controller is obtained by Eq.(8) and Eq.(12) we get,
21 21
21 2121 23 26
31 31
31 3141 43
51 52 53 55 5621 21
61 62 63 65 6621 21
21
41
51
61
0 1 0 0 0 0
0 0 0
0 0 0 1 0 0
0 0 0 0
0
0
0
0
A A A
d
A Adt
A A A A Au u
A A A A A
B
B
B
B
 
 
 
 
 
     
         
     
    
     
     
    
         




 


21
1 2 3
41
51
61
0 0
0
0 0
0
0
0
C
Pm Pm Pm
D
C
C
    
    
    
    
        
    
     
     
      
Where and are formed using Eq. (8) and
Eq.(12),
Applying controllability criterion to all three input matrix,
It should follow,
C= n [1 : 1 : 1]
Where n is size of new Jacobian matrix.
3. RESULTS AND DISCUSSION
Dynamic performance of power system is simulated using
MATLAB software package. Control variable parameters
are given in Appendix. The power system is analyzed with
and without incorporating TCPS FACTS device based
controller. Eigen values of power system without and with
facts device are shown in Table I and that of damping
controller in table II. Phase portrait and time domain
simulation is carried out for the operating condition
following a 1% step perturbation in mechanical power of
generator 2 and generator 3. The phase portrait and time
domain results are shown from fig. 4.1 to fig 5.8
Table -1: Eigen Values of Power System as per figure 1
Eigen Value Oscillating
frequency(Hz)
0.0000 13.3597i 2.1263
0.0000 8.6892i 1.3829
As seen in table 1, that the system is purely oscillatory as
there is no damping in the system.
With Step disturbance of 1% in turbine side of generator 2 is
made as per figure 1, the phase portrait and time domain
results so obtained are,
0 1 2 3 4 5 6 7 8
x 10
-3
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.04
del  21 (rad)
del21(rad/s)
Phase potrait state -varible ,del  21 and del  21
Fig-4.1 Phase portrait state variable , and ,
-2 -1 0 1 2 3 4 5
x 10
-3
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.04
del  31 (rad)
del31(rad/s)
Phase potrait state -variable ,del  31 and del  31
Fig-4.2 Phase portrait state variable , and ,
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 214
0 10 20 30 40 50 60
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.04
Time (s)
del21(rad/s)
del  21 response with time
Fig-4.3 Response of with time
0 10 20 30 40 50 60
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.04
Time (s)
del31(rad/s)
del  31 response with time
Fig-4.4 Response of with time
With Step disturbance of 1% in turbine side of generator 3 is
made as per figure 1, the phase portrait and time domain
results so obtained are,
0 1 2 3 4 5 6 7 8 9
x 10
-3
-0.06
-0.04
-0.02
0
0.02
0.04
0.06
del  31 (rad)
del31(rad/s)
phase potrait -state varible, del  31 and del  31
Fig-4.5 Phase portrait state variable, and
-2 -1 0 1 2 3 4
x 10
-3
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
del  21 (rad)
del21(rad/s)
Phase potrait state -variable, del  21 and del  21
Fig-4.6 Phase portrait state variable, and,
0 10 20 30 40 50 60
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
Time (s)
del21(rad/s)
del  21 response with time
Fig-4.7 Response of with time
0 10 20 30 40 50 60
-0.06
-0.04
-0.02
0
0.02
0.04
0.06
Time (s)
del31(rad/s)
del  31 response with time
Fig-4.8 Response of with time
It is clearly seen in figure 4.1 through 4.8, that as soon as
disturbance is created the system is unable to find new
equilibrium state due to lack of damping component. The
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 215
same can also be inferred from different responses of state
variables with time.
Through section 2 and 2.1, the eigen values were computed
and can be seen in table 2.
Table -2: Eigen Values of Power System as per figure 3
Eigen value Oscillating
frequency(Hz)
Zeta (
-48.6728 0 1
-.03281 13.0505i 2.0771 0.0251
-3.6319 8.2018i 1.3054 0.4049
-0.1010 0 1
As seen in table 2, that the system is now damped with zeta
lying within o and 1, and also it is to seen that the frequency
of oscillation has not changed much from previous value.
With Step disturbance of 1% in turbine side of generator 2 is
made as per figure 3, the phase portrait and time domain
results so obtained are,
0 0.5 1 1.5 2 2.5
x 10
-3
-0.015
-0.01
-0.005
0
0.005
0.01
0.015
del  31 (rad)
del31(rad/s)
Phase potrait- state varible,del  31 and del  31
Fig-5.1 Phase portrait state variable, and
0 0.5 1 1.5 2 2.5 3 3.5 4 4.5
x 10
-3
-5
0
5
10
15
20
x 10
-3
del  21 (rad)
del21(rad/s)
Phase potrait state -variable,del  21 and del  21
Fig-5.2 Phase portrait state variable, and
0 5 10 15 20 25 30
-0.015
-0.01
-0.005
0
0.005
0.01
0.015
0.02
Time (s)
del21anddel31
Response of del  21 and del  31 with time
A
B
A= and B= (rad/s)
Fig-5.3 Response of and with time
0 10 20 30 40 50 60
-5
0
5
10
15
20
x 10
-4
Time (s)
del21
del  21 response with time
Fig-5.4 Response of with time
With Step disturbance of 1% in turbine side of generator 3 is
made as per figure 3, the phase portrait and time domain
results so obtained are,
0 1 2 3 4 5 6 7 8
x 10
-3
-0.05
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.04
0.05
del  31 (rad)
del31(rad/s)
Phase potrait -state variable ,del  31 and del  31
Fig-5.5 Phase portrait state variable, and
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 216
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2
x 10
-3
-0.01
-0.008
-0.006
-0.004
-0.002
0
0.002
0.004
0.006
0.008
0.01
del  21 (rad)
del21(rad/s)
Phase potrait -state variable,del  21 and del  21
Fig-5.6 Phase portrait state variable, and
0 5 10 15 20 25 30
-0.05
-0.04
-0.03
-0.02
-0.01
0
0.01
0.02
0.03
0.04
0.05
Response of del  21 and del  31 with time
Time(s)
del21anddel31
A
B
A= and B= (rad/sec)
Fig-5.7 Response of and with time
0 10 20 30 40 50 60
-1
-0.8
-0.6
-0.4
-0.2
0
0.2
0.4
0.6
0.8
1
x 10
-3
Time (s)
del21
del  21 response with time
Fig-5.8 Response of with time
It is clearly seen in figure 5.1 through 5.8; section 2, 2.1,
that as soon as disturbance is created in the system
comprising of facts device is now able to find new
equilibrium state via presence of damping component as
evident in phase portrait available. The same can also be
inferred from different responses of state variables with
time.
3. CONCLUSIONS
In this paper steady state analysis of a multi machine power
system that is 3 machines and 9 bus power system about an
initial operating condition available from load flow is
analyzed. Multi machine power system is successfully
analyzed with and without TCPS FACTS device based
controller. The studies conducted in this paper yield the
following conclusions:
1. It is observed that, test power system without controller
is in purely oscillatory mode due to insufficient damping
in the system.
2. By incorporating TCPS FACTS device based controller
damping is introduced in system, damping of
electromechanical mode of oscillation and steady state
stability are enhanced by its usage.
3. The effectiveness of the control scheme for enhancement
in damping has been successfully analyzed through
eigen value analysis, phase portrait and time-domain
simulations of linearized model for an operating
condition.
REFERENCES
[1]. Divya Rishi Shrivastava, “Synchronizing and Damping
Effects of TCPS and TCSC Based Coordinated Damping
Controllers: Single Machine Infinite Bus”, IJLTEMAS, Vol.
III, Issue IX, September 2014.
[2]. K.R.Padiyar, “FACTS Controllers in Power
Transmission and Distribution”, New Age International
Limited, Publishers, 2013
[3]. Fernando Javier De Marco, Nelson Martins, and Julio
Cesar RezendeFerraz, “An Automatic Method for Power
System Stabilizers Phase Compensation Design”,IEEE
Trans. On power systems, vol. 28, no. 2, may 2013.
[4]. P. Kundur, “Power System Stability and Control”, Tata
McGraw-Hill,2012.
[5]. M. A. Abido, “Power System Stability Enhancement
Using Facts Controllers: A Review”, The Arabian
Journal for Science and Engineering, vol. 34, 2009.
[6]. “IEEE Guide for Synchronous Generator Modeling
Practice and Application in Power System Stability
Analysis”, IEEE Power Engineering Society, Sponsor,
April 2008.
[7]. IEEE/CIGRE Joint Task Force on Stability Terms and
Definitions, “Definition and Classification of Power System
Stability”, IEEE TRANSACTIONS ON Power Systems, VOL.
19, NO. 2, May 2004.
[8]. Paul M Anderson, A.A .Fouad , “ Power System
Control And Stability,”Wiley,IEEE press, October 2002.
[9]. N. G. Hingorani, L. Gyugyi, “Understanding FACTS
Concepts and Technology of Flexible AC Transmission
Systems”, IEEE Power Engineering Society, Sponsor,2000.
IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308
_______________________________________________________________________________________
Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 217
[10]. Ramnarayan Patel, T. S. Bhatti and D. P. Kothari,
“MATLAB/Simulink-based transient stability analysis of a
multimachine power system”,International Journal of
Electrical Engineering Education 39/4.
[11]. “IEEE Guide for Synchronous Generator Modeling
Practices in Stability Analyses”, IEEE Power Engineering
Society, Sponsor, March 21,1991.
[12]. Kai Xing, “Application of Thyristor-Controlled Phase
shifters to minimize real power losses and augment stability
of power systems”,IEEE transaction on Energy Conversion
,vol. 3,No. 4,December 1988
[13]. IEEE Symposium on “Proposed Terms and Definitions
For Power System stability”, IEEE Tran. On power
Apparatus and system.vol.PAS-101, no.7 July 1982
[14]. A. M. Liapunov, “The general problem of the stability
of motion”, 1892.
[15]. A. Chipperfield, P. Fleming, H. Pohlheim, C. Fonseca,
“Genetic Algorithm TOOLBOX for Use with MATLAB”,
Mathworks.in.
[16]. NPTEL Online, “Power System Analysis”, Module 4,
IIT Kanpur, NPTEL.
Appendix I (generator data)
Generator 1 2 3
Rated MVA 247.5 192 128
kV 16.5 18 13.8
Power factor 1.0 0.85 0.85
Type Hydro Steam Steam
Speed 180r/min 3600r/min 3600r/min
0.1460 0.8958 1.3125
0.0608 0.1198 0.1813
0.0969 0.8645 1.2578
0.0969 0.1969 0.25
(leakage) 0.0336 0.0521 0.0742
8.96 6.00 5.89
0 0.535 0.600
Stored energy
at rated speed
2364 MW
.s
640 MW.s 301 MW.s
Reactance values are in pu on a 100-MVA base
Appendix II. (Reduced Y Matrix)
Appendix III. (Synchronizing components, For Figure 1)
0 2.0511 1.6139
1.8329 0 1.3016
1.5005 1.3641 0
 
 
 
  
Appendix IV. (Controller parameters)
T1=0.017s T2=0.02s =10s K=0.1
Appendix V. (Synchronizing components, For Figure 3)
0 1.6971 1.3357
1.5060 0 1.1281
1.2508 1.1803 0
 
 
 
  
BIOGRAPHIES
Divya Rishi Shrivastava (M’26) is
Assistant Professor in Electrical &
Electronics Engineering Dept., Manipal
University Jaipur, Rajasthan, India. He
received M.Tech. in 2014 from NIT
Silchar, India
Daneshwari R Akkishetti (F’22) is lecturer
in Electrical & Electronics Engineering
department, Jain College of Engineering
Belgaum Karnataka, India. She received
B.E. degree in 2015 from JCE, Belgaum,
VTU, India.

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Steady state stability analysis and enhancement of three machine nine bus power system using tcps facts device

  • 1. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 210 STEADY STATE STABILITY ANALYSIS AND ENHANCEMENT OF THREE MACHINE NINE BUS POWER SYSTEM USING TCPS FACTS DEVICE Divya Rishi Shrivastava1 , Daneshwari R Akkishetti 2 1 Assistant Professor, Electrical & Electronics Dept., Manipal University Jaipur, Rajasthan, India 2 Lecturer, Electrical & Electronics Dept., Jain College of Engineering Belgaum, Karnataka, India Abstract Power System stability study is the important parameter of economic, reliable and secure system planning and operation. Studies are important during the planning and conceptual design stages of the project as well as during the operating life of the plant periodically. This paper presents the power system steady state stability analysis for IEEE- 9 bus test system and examines influence of TCPS FACTS device based controller on test system. It is assumed that system under study has been perturbed from a steady state equilibrium that prevailed prior to the application of the disturbance. If system is stable, we would expect that for temporary or permanent disturbance, system will acquire initial or new operating state after a transient period. The stability study is accessed using Lyapunov’s first method. The effectiveness of damping controller in enhancing the steady state stability is investigated by incorporating available constraints. For analysis MATLAB software is employed. The conclusions have been drawn here, based on theoretical and mathematical analysis so as to provide an insight and better understanding of steady state stability of considered multi machine power system. Key Words: Lyapunov’s first method, Steady-state stability, Phase portrait, FACTS device, supplementary modulation controller, eigen value, synchronizing power coefficient, IEEE-9 Bus Test System, Load Flow Study, Differential algebraic equation. --------------------------------------------------------------------***---------------------------------------------------------------------- 1. INTRODUCTION Power system stability may be defined as property of a power system that enables it to remain in a state of operating equilibrium under normal operating conditions and to regain an acceptable state of equilibrium after being subjected to a disturbance [4]. The oscillations, which are typically in the frequency range of 0.2 to 3.0 Hz, might be excited by the disturbances in the system [1][13] or, in some cases, might even build up spontaneously. A power system at a given operating condition may be unstable due to large disturbance; still such a system can be operated, though insecurely. However, if the system is small signal unstable at a given operating condition, it cannot be operated. Therefore, steady state stability is a fundamental requirement for satisfactory operation of power system. Instability that may result can be of two forms i)increase in rotor angle through a non-oscillatory or aperiodic mode due to lack of synchronizing torque, or ii)rotor oscillation of increasing amplitude due to lack of sufficient damping torque[13].With the advent of FACTS devices, and due to recent advances in power electronics , its capability to enhance oscillation damping and system stability has been explored as potential application. With advent of high power, high speed electronic FACTS controllers have been mainly used for solving various power system control problems such as voltage regulation, power flow, and transfer capability enhancement. As supplementary functions, they have been in use for damping the inter area modes and enhancing power system stability [3]. This paper studies theoretical and mathematical analysis of IEEE 3- machine – 9 bus power system and the influence of the TCPS FACTS device based controller on the steady state stability about an operating condition. Here, controller parameters are obtained by incorporating available constraints. The Mathematical analysis is carried out in MATLAB using eigenvalue analysis, phase portrait and time domain analysis of state variable of power system when subjected to small disturbance. 1.1 IEEE -3 Machine 9 Bus Power System We have considered the popular Western System Coordinated Council (WSSC), IEEE 3-machine, 9-bus system shown in fig.1. This system is also appearing in references [8] and [10].The base MVA is 100 and system frequency is 60Hz. The system data are given in Appendix I. Classical model of the generators are employed for analysis. The operating conditions are obtained by using Load flow analysis. Eigen value analysis and phase portrait for concerned state variable are drawn about available operating state. The Enhancement in steady state stability is analyzed by incorporating TCPS FACTS device based controller, the gains of which are taken by incorporating available constraints. For Analysis TCPS FACTS device is placed between Machine 1 and 2.
  • 2. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 211 1.2 Mathematical Model A load flow study of a power system shown in Fig. 1, is done to determine electrical power output of machine i and to calculate values of for all generators. Fig-1 IEEE 3-machine 9-bus power system The power into the network at node i, (1) Where, = negative of the transfer admittance between nodes i and j. = driving point admittance for node i. Once Y matrix is calculated, we eliminate all the nodes expect for the internal generator nodes and obtain the Y matrix for reduced network. The reduction can be achieved by matrix operation considering fact that all the nodes have zero injection currents except for the internal generator nodes. In a power system with n generators, the nodal equation can be written as, (2) Where subscript n is used to denote generator nodes and subscript r is used for the remaining nodes. Expanding Eq. (2) 0= From which we eliminate to find ) ) (3) It has dimensions ( where n is the number of generators. This convenient analytic technique that can be used only when the loads are treated as constant impedance [8][11]. The equation of motion for i th machine given by, + (4) (5) The electrical power is given by Eq.(1). Linearizing Eq.(1) and (5) about initial operating condition [4] represented by = yields, (6) defined as synchronizing power coefficient [4]. The test power system is now linearized about initial operating condition available from load flow. The classical model [6][7]of a synchronous machine is used to study the stability of a power system. Linearizing multi machine system about an initial operating condition using equations (4) and (5) gives, (7) When generator 2 and 3 are swinging with respect to generator 1,
  • 3. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 212 (8) From Eq. (8) the state space representation of the test system is given by, 21 21 21 21 23 21 1 1 31 31 31 41 43 31 1 2 2 3 3 0 1 0 0 0 0 0 / 2 0 0 0 1 0 0 0 / 2 0 0 / 2 0 0 / 2 0 0 r r r r A A w Hd Pm dt A A w H w H Pm Pm w H                                                                                          (9) Where Eq. are formed using Eq. (8). Eq. (9) is written in standard control theory form , where X is state variable vector and U is the control variable vector. Applying controllability criterion to all three input matrix, It should follow, C=n [1 : 1 : 1] Where n is size of Jacobian matrix. 2.TCPS FACTS DEVICE BASED CONTROLLER MODELLING Thyristor controlled phase shifter is used to enhance steady state stability of power system. TCPS FACTS device based controller enable fast control of the phase angle ( and it is determined as non linear function of rotor angle and speed. It is used to damp low frequency oscillation. For TCPS FACTS device based damping controller generally Supplementary Modulation Controller are recommended [2],by designing a SMC for the damping controller based on rotor speed signal as input, it is possible to enhance the damping and stabilize swing mode. TCPS FACTS device based controllers are based on conventional lead-lag type. Here and provide the required phase compensation to give necessary damping. is washout circuit time constant, wash out circuit serves as a high pass filter with time constant varies from 10s to 20s [2]. Fig-2 Structure of TCPS based controller Controllable parameter of the TCPS FACTS device based controller is that is rotor angle of generator and the control law is, The transfer function of controller is given by, (10) Differential algebraic equation of damping controller can be formulated from Eq.(10) (11) Here, controller parameters are obtained by incorporating available constraints such as, i) No new mode of oscillation should evolve ii) Damping in the system that should be,0< ζ ≤ 1 iii) All states variables should be controllable 2.1 Mathematical Modelling IEEE 9 Bus Power System with TCPS Facts Device Fig-3 Reduced figure 1 with damping controller The test power system is equipped with TCPS FACTS device based controller near generator terminal between bus 2 and 1 as shown in Fig.3. As losses of the thyristors are a
  • 4. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 213 small proportion of the DC link power and quadrature power inserted by transformer is small proportion of the line primary power so that phase shifter losses are neglected [12] and Time constant of thyristors is very short; and can be neglected for computation [12]. The dynamic equation of system with damping controller are obtained by Eq. (8) and (11), linearizing these equations about operating point we get, (12) The state space representation of test system with damping controller is obtained by Eq.(8) and Eq.(12) we get, 21 21 21 2121 23 26 31 31 31 3141 43 51 52 53 55 5621 21 61 62 63 65 6621 21 21 41 51 61 0 1 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 A A A d A Adt A A A A Au u A A A A A B B B B                                                                         21 1 2 3 41 51 61 0 0 0 0 0 0 0 0 C Pm Pm Pm D C C                                                      Where and are formed using Eq. (8) and Eq.(12), Applying controllability criterion to all three input matrix, It should follow, C= n [1 : 1 : 1] Where n is size of new Jacobian matrix. 3. RESULTS AND DISCUSSION Dynamic performance of power system is simulated using MATLAB software package. Control variable parameters are given in Appendix. The power system is analyzed with and without incorporating TCPS FACTS device based controller. Eigen values of power system without and with facts device are shown in Table I and that of damping controller in table II. Phase portrait and time domain simulation is carried out for the operating condition following a 1% step perturbation in mechanical power of generator 2 and generator 3. The phase portrait and time domain results are shown from fig. 4.1 to fig 5.8 Table -1: Eigen Values of Power System as per figure 1 Eigen Value Oscillating frequency(Hz) 0.0000 13.3597i 2.1263 0.0000 8.6892i 1.3829 As seen in table 1, that the system is purely oscillatory as there is no damping in the system. With Step disturbance of 1% in turbine side of generator 2 is made as per figure 1, the phase portrait and time domain results so obtained are, 0 1 2 3 4 5 6 7 8 x 10 -3 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 del  21 (rad) del21(rad/s) Phase potrait state -varible ,del  21 and del  21 Fig-4.1 Phase portrait state variable , and , -2 -1 0 1 2 3 4 5 x 10 -3 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 del  31 (rad) del31(rad/s) Phase potrait state -variable ,del  31 and del  31 Fig-4.2 Phase portrait state variable , and ,
  • 5. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 214 0 10 20 30 40 50 60 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 Time (s) del21(rad/s) del  21 response with time Fig-4.3 Response of with time 0 10 20 30 40 50 60 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 Time (s) del31(rad/s) del  31 response with time Fig-4.4 Response of with time With Step disturbance of 1% in turbine side of generator 3 is made as per figure 1, the phase portrait and time domain results so obtained are, 0 1 2 3 4 5 6 7 8 9 x 10 -3 -0.06 -0.04 -0.02 0 0.02 0.04 0.06 del  31 (rad) del31(rad/s) phase potrait -state varible, del  31 and del  31 Fig-4.5 Phase portrait state variable, and -2 -1 0 1 2 3 4 x 10 -3 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 del  21 (rad) del21(rad/s) Phase potrait state -variable, del  21 and del  21 Fig-4.6 Phase portrait state variable, and, 0 10 20 30 40 50 60 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 Time (s) del21(rad/s) del  21 response with time Fig-4.7 Response of with time 0 10 20 30 40 50 60 -0.06 -0.04 -0.02 0 0.02 0.04 0.06 Time (s) del31(rad/s) del  31 response with time Fig-4.8 Response of with time It is clearly seen in figure 4.1 through 4.8, that as soon as disturbance is created the system is unable to find new equilibrium state due to lack of damping component. The
  • 6. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 215 same can also be inferred from different responses of state variables with time. Through section 2 and 2.1, the eigen values were computed and can be seen in table 2. Table -2: Eigen Values of Power System as per figure 3 Eigen value Oscillating frequency(Hz) Zeta ( -48.6728 0 1 -.03281 13.0505i 2.0771 0.0251 -3.6319 8.2018i 1.3054 0.4049 -0.1010 0 1 As seen in table 2, that the system is now damped with zeta lying within o and 1, and also it is to seen that the frequency of oscillation has not changed much from previous value. With Step disturbance of 1% in turbine side of generator 2 is made as per figure 3, the phase portrait and time domain results so obtained are, 0 0.5 1 1.5 2 2.5 x 10 -3 -0.015 -0.01 -0.005 0 0.005 0.01 0.015 del  31 (rad) del31(rad/s) Phase potrait- state varible,del  31 and del  31 Fig-5.1 Phase portrait state variable, and 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 x 10 -3 -5 0 5 10 15 20 x 10 -3 del  21 (rad) del21(rad/s) Phase potrait state -variable,del  21 and del  21 Fig-5.2 Phase portrait state variable, and 0 5 10 15 20 25 30 -0.015 -0.01 -0.005 0 0.005 0.01 0.015 0.02 Time (s) del21anddel31 Response of del  21 and del  31 with time A B A= and B= (rad/s) Fig-5.3 Response of and with time 0 10 20 30 40 50 60 -5 0 5 10 15 20 x 10 -4 Time (s) del21 del  21 response with time Fig-5.4 Response of with time With Step disturbance of 1% in turbine side of generator 3 is made as per figure 3, the phase portrait and time domain results so obtained are, 0 1 2 3 4 5 6 7 8 x 10 -3 -0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05 del  31 (rad) del31(rad/s) Phase potrait -state variable ,del  31 and del  31 Fig-5.5 Phase portrait state variable, and
  • 7. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 216 0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2 x 10 -3 -0.01 -0.008 -0.006 -0.004 -0.002 0 0.002 0.004 0.006 0.008 0.01 del  21 (rad) del21(rad/s) Phase potrait -state variable,del  21 and del  21 Fig-5.6 Phase portrait state variable, and 0 5 10 15 20 25 30 -0.05 -0.04 -0.03 -0.02 -0.01 0 0.01 0.02 0.03 0.04 0.05 Response of del  21 and del  31 with time Time(s) del21anddel31 A B A= and B= (rad/sec) Fig-5.7 Response of and with time 0 10 20 30 40 50 60 -1 -0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.8 1 x 10 -3 Time (s) del21 del  21 response with time Fig-5.8 Response of with time It is clearly seen in figure 5.1 through 5.8; section 2, 2.1, that as soon as disturbance is created in the system comprising of facts device is now able to find new equilibrium state via presence of damping component as evident in phase portrait available. The same can also be inferred from different responses of state variables with time. 3. CONCLUSIONS In this paper steady state analysis of a multi machine power system that is 3 machines and 9 bus power system about an initial operating condition available from load flow is analyzed. Multi machine power system is successfully analyzed with and without TCPS FACTS device based controller. The studies conducted in this paper yield the following conclusions: 1. It is observed that, test power system without controller is in purely oscillatory mode due to insufficient damping in the system. 2. By incorporating TCPS FACTS device based controller damping is introduced in system, damping of electromechanical mode of oscillation and steady state stability are enhanced by its usage. 3. The effectiveness of the control scheme for enhancement in damping has been successfully analyzed through eigen value analysis, phase portrait and time-domain simulations of linearized model for an operating condition. REFERENCES [1]. Divya Rishi Shrivastava, “Synchronizing and Damping Effects of TCPS and TCSC Based Coordinated Damping Controllers: Single Machine Infinite Bus”, IJLTEMAS, Vol. III, Issue IX, September 2014. [2]. K.R.Padiyar, “FACTS Controllers in Power Transmission and Distribution”, New Age International Limited, Publishers, 2013 [3]. Fernando Javier De Marco, Nelson Martins, and Julio Cesar RezendeFerraz, “An Automatic Method for Power System Stabilizers Phase Compensation Design”,IEEE Trans. On power systems, vol. 28, no. 2, may 2013. [4]. P. Kundur, “Power System Stability and Control”, Tata McGraw-Hill,2012. [5]. M. A. Abido, “Power System Stability Enhancement Using Facts Controllers: A Review”, The Arabian Journal for Science and Engineering, vol. 34, 2009. [6]. “IEEE Guide for Synchronous Generator Modeling Practice and Application in Power System Stability Analysis”, IEEE Power Engineering Society, Sponsor, April 2008. [7]. IEEE/CIGRE Joint Task Force on Stability Terms and Definitions, “Definition and Classification of Power System Stability”, IEEE TRANSACTIONS ON Power Systems, VOL. 19, NO. 2, May 2004. [8]. Paul M Anderson, A.A .Fouad , “ Power System Control And Stability,”Wiley,IEEE press, October 2002. [9]. N. G. Hingorani, L. Gyugyi, “Understanding FACTS Concepts and Technology of Flexible AC Transmission Systems”, IEEE Power Engineering Society, Sponsor,2000.
  • 8. IJRET: International Journal of Research in Engineering and Technology eISSN: 2319-1163 | pISSN: 2321-7308 _______________________________________________________________________________________ Volume: 04 Issue: 12 | Dec-2015, Available @ http://www.ijret.org 217 [10]. Ramnarayan Patel, T. S. Bhatti and D. P. Kothari, “MATLAB/Simulink-based transient stability analysis of a multimachine power system”,International Journal of Electrical Engineering Education 39/4. [11]. “IEEE Guide for Synchronous Generator Modeling Practices in Stability Analyses”, IEEE Power Engineering Society, Sponsor, March 21,1991. [12]. Kai Xing, “Application of Thyristor-Controlled Phase shifters to minimize real power losses and augment stability of power systems”,IEEE transaction on Energy Conversion ,vol. 3,No. 4,December 1988 [13]. IEEE Symposium on “Proposed Terms and Definitions For Power System stability”, IEEE Tran. On power Apparatus and system.vol.PAS-101, no.7 July 1982 [14]. A. M. Liapunov, “The general problem of the stability of motion”, 1892. [15]. A. Chipperfield, P. Fleming, H. Pohlheim, C. Fonseca, “Genetic Algorithm TOOLBOX for Use with MATLAB”, Mathworks.in. [16]. NPTEL Online, “Power System Analysis”, Module 4, IIT Kanpur, NPTEL. Appendix I (generator data) Generator 1 2 3 Rated MVA 247.5 192 128 kV 16.5 18 13.8 Power factor 1.0 0.85 0.85 Type Hydro Steam Steam Speed 180r/min 3600r/min 3600r/min 0.1460 0.8958 1.3125 0.0608 0.1198 0.1813 0.0969 0.8645 1.2578 0.0969 0.1969 0.25 (leakage) 0.0336 0.0521 0.0742 8.96 6.00 5.89 0 0.535 0.600 Stored energy at rated speed 2364 MW .s 640 MW.s 301 MW.s Reactance values are in pu on a 100-MVA base Appendix II. (Reduced Y Matrix) Appendix III. (Synchronizing components, For Figure 1) 0 2.0511 1.6139 1.8329 0 1.3016 1.5005 1.3641 0          Appendix IV. (Controller parameters) T1=0.017s T2=0.02s =10s K=0.1 Appendix V. (Synchronizing components, For Figure 3) 0 1.6971 1.3357 1.5060 0 1.1281 1.2508 1.1803 0          BIOGRAPHIES Divya Rishi Shrivastava (M’26) is Assistant Professor in Electrical & Electronics Engineering Dept., Manipal University Jaipur, Rajasthan, India. He received M.Tech. in 2014 from NIT Silchar, India Daneshwari R Akkishetti (F’22) is lecturer in Electrical & Electronics Engineering department, Jain College of Engineering Belgaum Karnataka, India. She received B.E. degree in 2015 from JCE, Belgaum, VTU, India.