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Chaotic Oscillationofa Three-bus Power System Model 
Using ElmanNeural Network 

 
I Made Ginarsa1, Adi Soeprijanto2, Mauridhi Hery Purnomo3 

1Dept. of Electrical Engineering, Mataram University, Mataram 
2Dept. of Electrical Engineering, Sepuluh Nopember Institute of Technology, Surabaya 
3Dept. of Electrical Engineering, Sepuluh Nopember Institute of Technology, Surabaya 

e-mail: kadekgin@yahoo.com1, adisup@ee.its.ac.id2, hery@ee.its.ac.id3 
 
 

Abstrak 
 
Paper ini meneliti dan membahas secara mendalam mengenai osilasi chaotic pada sistem 
tenaga listrik.Dengan menggunakan sebuah three-bus pada sistem tenaga listrik, rute mungkin 
menyebabkan unjuk kerja chaotic sehingga dievaluasi, digambarkan serta dibahas dalam 
penelitian ini. Osilasi chaotic ini dimodelkan menggunakan Elmanneural network  karena 
bentuknya yang sederhana dan juga melibatkan algoritmabackpropagation dengan adaptive 
learning rate dan momentumnya.Unjuk kerja learning rate dan momentumnya lebih baik 
dibandingkan jika tanpa momentumnya. Unjuk kerja chaotic dalam sistem tenaga listrik muncul 
karena sistem ini dioperasikan dalam mode critical. Unjuk kerja chaotic ini terdeteksi dengan 
munculnya sebuahchaotic attractordalam phase-plane trajectory. 
 
Kata kunci:sistem tenaga listrik, Elman neural network, chaotic attractor, phase-plane trajectory 

 
Abstract 

 
Chaotic oscillation of power systems was deeply studied in this paper. By using a three-bus 
power system, route may cause chaotic behavior in power systems are evaluated, illustrated 
and discussed.Chaotic oscillationof power systems was modeled using Elman neural network 
because the Elman neural networkhas a simple form. Backpropagation algorithm with adaptive 
learning rate and momentum was proposed in this research. Performance of learning rate with 
momentum was better than learning rate without momentum. Chaoticbehaviors in a power 
system appeared due to the system operated in critical mode. A Chaotic behavior in power 
systems was detected by appearing a strange attractor (a chaotic attractor) in phase-plane 
trajectory. 
 
Keywords:power systems, Elman neural network, chaotic attractor, phase-plane trajectory 

 
 

1. Introduction 
 

In recent years, electric power consuming has grown up rapidly. On the other hand, the power 
plants and transmission systems being built are very slow due to environmentaland economical 
constraints. This condition will make the power systems operate in critical mode at the boundary 
of stability region. Meanwhile, chaotic phenomena is one type of un-deterministic oscillations 
exist in deterministic systems such as in power system model.Chiang et al, have builtvoltage 
collapse model, both physical explanations and computational considerations of this model are 
presented. Static and dynamic models are used to explain the type of voltage collapse, where 
the static is used before a saddle-node bifurcation and the dynamic model is employed after the 
bifurcation [1]. Lyapunov exponent, measuring how rapidly two nearby trajectories separate 
from one another within state space and broad-band spectrum was used to confirm the 
observation [2]. Within the range of loading conditions, the sensitive dependence feature of 
chaotic behaviors makes the power system unpredictable after a finite time. In addition, within 
the range the effectiveness any control scheme was questionable and should bere-evaluated 
based on state vector information.Furthermore,nonlinear phenomena including bifurcation, 
chaos and voltage collapse occurred in a power system model. The present of the various 
nonlinear phenomena was found to be a crucial factor in the inception of voltage collapse in this 



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model. The problem of controlled and suppressed of the presence of non-linear phenomena in 
power systems were addressed here in this paper. The bifurcation control approach is approach 
to modify the bifurcations and to suppress chaos [3,4]. The presence of chaos in a power 
system causing seriously unstable problem was studiedby Yu, et al.[5]. The existence chaos in 
power systems due to disturbing of energy at rotor speed has been found in Ref.[6]. One 
scheme of chaos utility was used on electrical systems for smelting which was based on chaos 
control. Lei et al. Demonstratedthat chaotic steel-smelting ovens regulate their heating current 
according to chaos control theory [7]. A control system using a neural network controller was 
presumed to be able to stabilize the unstable focus points of 2-dimensional chaotic systems; 
although, Konishiand Kokame stated that the control system did not require this presumption 
[8]. Elman neural network was used to predict short-term load forecasting in power systems [9]. 
Modeling of chaotic behavior using RNN has been studied in [10]. Various studies on controlling 
transient chaos have been carried out, such as those by Dhamala et al., and Dhamala and Lai 
attempted to control transient chaos in power systems using a data time series [11,12]. 
Strategies for controlling chaos in process plants have been tested on the Henon mapdiscrete 
chaotic system [13]. 
 
In this paper, we focused on the cause of chaotic oscillation in power systems and its model. By 
using Elman neural network model is proposed. The reason of using the Elman neural network 
because the Elman network is able to traindata both on present input and on past output, and 
other reason because an Elman RNN has simple form. 
 
This paper is organized as follows: in advance, power system model used in this research is 
given in Section 2. Then, Elman neural network model isexplained in Section 3. Chaotic 
behavior due to sensitivityof initialcondition and analysis a chaotic behavior are presented in 
Section 4 and 5, respectively. The conclusionis given in the last section. 

2.  Power System Model 
 
A Synchronous machine was modeled as a voltage (Eq0’) behind a direct reactance (xd’). The 
voltage magnitude was assumedas remaining constant at the pre-disturbance value, as shown 
in Fig.1(a).De Mello and Concordia as well as Padiyar and Kundur derivedof a machine 
connected toan infinite bus [13,14]. Meanwhile, if saturation and the stator resistance were 
neglected, the system condition was balanced with a static load. The mechanical mode block 
diagram of single-machine connected to infinite bus is shown in Fig.1(b). 
 

 

 
Figure 1.Single machine connected to infinite bus. 

(a) Circuit equivalent (b)Mechanical mode. 
  



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The machine wasconnected to infinite bus and supplied the load. Then the armature current 
flowedfrom the machine to the load. This current causedelectrical torque on the stator winding, 
and vice versa. The mechanical torque was produced by flux through the rotor winding. 
Meanwhile, whenthe rotor speed wasconstant, the rotor speed followed thesynchronous speed. 
When there was imbalanced energy, the rotor speed accelerated or decelerated and caused the 
swing equation.The swing equation is represented as follows: 

 

ema TTTDH      (1) 
 

Where D, are  amping constant and rotor speed deviation, respectively.  Eq.1 is a basic 
equation for mechanical modeof single machine connected to infinite bus. Furthermore,the the 
Eq. 1 can be expressed as follows: 

 

B       (2) 

DTT
M em
1

(3)    

Where Tm, Te, , , D and M are mechanical torque, electrical torque, power angle, speed 
rotor, damping constant, inertia constant respectively.The system was developed from Ref.[3] 
and shown in Fig.3, which is regarded as one synchronous machine supplying power to a local 
dynamic load shunt with a capacitor (Bus 2) and connected by weak tie line to the extern 
system (Bus 3). The system equations are: 
 

.      (4) 

881.1..333.3
087.0sin667.16

d
VLL       (5)  

333.43333.33
209.0cos667.666

333.93
087.0cos667.166

872.496

1

2

d

LL

L

LL

LL

Q
V

V
V

V

(6)   

033.7229.5
135.0cos869.104523.14

012.0cos217.26
764.78

1

2

d

LL

LL

LL

Q
V

V
VV

  (7) 

 

Table 1. Power system parameters 
Y0 Ym 0 m V0 Vm Pm M 
20.
0 

5.0 5.
0 

5.
0 

1.0 1.0 1.0 0.3 

D T C Kp  Kpv Kq  Kqv Kqv2 
0.0
5 

8.5 12.
0 

0.4 0.3 0.0
3 

2.
8 

2.1 

 
 



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Figure 2.One line diagram power system with 3 buses. 

, , d, Qld, L,VL, arethe power angle, rotor speed deviation, damping constant, reactive load, 
voltage angle and  magnitude at load bus, respectively. Eqs.4,5,6,and7 can be simplified into a 
uniform equation in Eq.8. 

 
pn RRxxfx ,,, ,     (8) 

 
Where x is vector state variables and  is vector of parameters. The state variables are x = 
[ , , L,VL]

T, superscript T denote transpose of the associate vector. 
 

3.  ElmanNeural Network Model 
 
Recurrent Elman network commonly is a two-layer network with feedback from the first-layer 
output to the first-layer input. This recurrent connection allows the Elman network to both detect 
and generate time-varying patterns. A two-layer Elman network is shown in Fig.3. The Elman 
network has tansig neurons in its hidden (recurrent) layer and purelin in its output layer. The 
Elman network differs fromconventional two-layer networks in that the first layer has a recurrent 
connection. The delay in this connection stores values from the previous time step, which can 
be used in the current time step. Thus, even if two Elman networks with the same weight and 
bias, are given identical inputs at a given time step, their outputs can be different due to different 
feedback states. Because network can store information for future reference, it is able to learn 
temporal pattern as well as spatial patterns [15,16,17,18]. The Elman network can be trained to 
respond and to generate, both kinds of patterns. 

 

2
1

1,2
2

1
1

1,11,1
1 1tansig

bnaLWpurelinna

bnaLWpIWna
.     (9) 

 
The architecture 4:8:8:4 RNN is used in this research. Where p,a1(n), a2(n), IW1,1, LW1,1, LW1,2, 
b1 and b2 are the vector input, recurrent-layer output, purelin-layer output, weight first-layer, 
weight hidden layer back to first-layer, weight hidden layer to output layer and biases, 
respectively. 

 
Figure 3.Elman recurrent neural network block diagram[18] 

 



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The RNN wastrained by using 1000 data points. Tansig and purelin activation function were 
used at hidden layer and at output layer, respectively. Data time series were obtained from the 
mathematical (exact) model in Eqs.4-7, respectively. The network performance is measured by 
mean square error (MSE). Formula of the MSE can be expressed by equation as follow: 
 

k

i
nn xxk

MSE
1

2ˆ1      (10) 

 
Where k, nx  and nx̂  are the size ofdata, input and estimation n

th data. 
 

4. Chaotic Behavior due to Sensitivity of InitialCondition 
 
Chaos definition and its properties have been given by Devaney and Alligood et al.[19,20]. 
Sensitivity of initial condition is one type of chaos properties. It is described by existing route to 
chaotic behavior in power systems caused by sensitivity of initial condition rotor speed ( 0). 
Initial rotor speed ( 0) in power systems was presented by disturbing ofenergy (DE). Kinetic 
energy disturbance was related to rotor speed deviation only. The large rotor speeddeviation 
was implemented as a large DE. When DE was smaller than the value of 1.3824 rad/s 
( 0<1.3824 rad/s)a power system converged to a stable equilibrium point. When the DE was 
increased, the convergencebecame more difficult. At 0 = 1.3825 rad/s, power systems 
produced route to a chaotic behavior in a longer time.When the DE was from1.3825 to 17003 
rad/s, the final states were controlled by a chaotic behavior. Furthermore, while the DE excess 
than 1.7004 rad/s the system went to divergence or voltage collapse. Based on the simulation 
result it is shown that chaotic behavior in power systems due todisturbing of energy at the rotor 
speed deviation. 

 
Table 2. System conditionwith different initial rotor speed ( 0) 

0(rad/s) Times (s) Final state Time response 
0.5 1000 Equilibrium point Fig.4(a) 

1.3824 1000 Equilibrium point Fig.4(b) 
1.3825 1000 Chaotic Fig.5(a) 
1.7003 1000 Chaotic Fig.5(b) 
1.7004 10 Divergen - 

 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 

Figure 4.Simulation results with equilibrium point state 
 



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Figure 5.Simulation results with chaotic state 

 

 
Figure 6. (a).Chaotic behavior of the rotor speed deviation 

(b). Magnified of Fig. 5 fromtime = 0 to time = 50 s 
 

5. Result and Analysis 
 
In this research, RNN initial simulation parameters were taken: learning rate train parameter = 
0.17; increment learning rate = 1.2; decrement learning rate = 0.6; and momentum learning rate 
= 0.75. The training performance of RNN using adaptive learning rate and adaptive learning rate 
with momentum are listed in Table 3.The training process is organized as follows: performances 
(MSE) are obtained to 14.7001 10 4 and 4.2209 10 4 at disturbance 0 = 0.5 rad/s for algorithm 
backpropagation adaptive learning rate (traingda) and backpropagation learning rate algorithm 
with momentum (traingdx),respectively. Moreover,performances were obtained to 16.8361 10 4 
and 4.6115 10 4 at disturbance 0 1.3825 rad/s. Furthermore, performances were obtained to 
17.4185 10 4 and 4.9442 10 4at the disturbance 0at the value of 1.7003 rad/s. During the 
training process the best performancewas obtained to 4.2209 10 4 at the disturbance of 0.5 
rad/s. 
  



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Figure 7. The chaotic behavior of the at 0 =1.7003 rad/s 
(a). Blue = exact model; red = RNN model (b). Error signal ofthe  

 
Figs.7-9 show the time responses of an exact and Elman recurrent neural network (RNN) 
model. Fig.7(a) shows rotor speed deviation ( ) time response which was oscillated due to the 
disturbance occurred at 01.7003 rad/s. Rotor speed oscillations exist in range from 1.6052 to 
1.5679 rad/s and from 1.511 to 1.6045 for the exact and RNN, respectively. Fig. 7(b) shows 
error signal of the rotor speed deviation; where the error signal is the difference of the exact and 
RNN model of the rotor speed deviation. 
 
Voltage angle ( L) at Bus 2 is affected by disturbing of energy (DE) at generator bus ( 00.5 
rad/s). The oscillation on voltage angle occurred at generator bus in a few second,then this 
oscillation decreased gradually and route to equilibrium point (fixed point) at point of 0.1128and 
0.1116 rad for exact and RNN models, respectively. The error signal of the voltage angle was 
measured by mean square error (MSE = 3.8193%), and these results are shown in Table 4. 
 
 

 
 

Figure 8.The chaotic behavior of the voltage angle when 0 at 1.7003 rad/s. 
(a). Blue = exact; red = RNN (b). Error signal of the L 

 
 



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Figure 9. The voltage magnitude (VL) time response at 0 = 1.7003 rad/s 
(a). Blue = exact model; red = RNN model (b). Error signalof the VL 

 
The voltage angle oscillation increased at the disturbance 1.3825, 1.600 and 1.7003 rad/s for 
exact model with amplitude in ranges (0.0600 to 0.1995 rad), (0.0351 to 0.2730rad), (0.0345 to 
0.2748rad) and (0.0340 to 0.2756rad), respectively. And the oscillation for RNN model arefrom 
0.0501 to 0.1879 rad, from 0.0460 to 0.2644rad, from 0.0332 to 0.2618radand from 0.0342 to 
0.2613rad, respectively. This oscillation occurred in a longer time. Voltage angle time response 
occurring at disturbance 01.7003 rad/s can be shown in Fig. 8. 
 
When the disturbance ( 0) at the value of 0.5 rad/s,the voltage magnitude oscillated in a few 
seconds. Furthermore, its decreased gradually route to equilibrium state (fixed point) at point 
1.095 pu and 1.008 for exact and RNN model, respectively. By increasing disturbance at 0 
1.3824 rad/s voltage magnitude is oscillated in a longer time in ranges (0.9967 to 1.1207pu) and 
then amplitude reduced and fixed point at 1.1095 pu (1520 s). 
 
On the opposite, when the disturbing of energy was increased up to 1.3825, 1.600 and 1.7003 
rad/s, voltage magnitude oscillated for the exact model where the amplitude increased 
from0.8307 to 1.1220pu, from0.8285 to 1.1118puand from 0.8290 to 1.1119pu, respectively. 
And the oscillation for RNN model was in the ranges from 0.8497 to 1.1158pu, from 0.8580 to 
1.1235puand from 0.8642 to 1.1185pu, respectively.In Fig.9, we can show that the voltage 
magnitude of the exact and RNN modelsexhibit chaotic behavior. 

 
Table 3.Performance of training algorithm using learningrate momentum 

0 
(rad/s) 

Training Times (s) 
102 

Performances 
MSE ( 10-4) 

traingda traingdx traingda traingdx 
0.5 69.3861 37.403 14.7001 4.2209 

1.3824 68.3250 42.342 17.2014 4.9080 
1.3825 67.3329 36.750 16.8361 4.6115 
1.7003 70.5781 41.840 17.4185 4.9442 

 
State trajectory(orbit) of the against is shown in Fig.10, where many circlesare made by 
themselves with boundary ranges from 1.6011 to +1.5535 rad/sandfrom 0.1165 to +0.7583 rad 
for the min- maxand min- max, respectively. Thestate trajectoriesofthe RNN model are made in 
rangesfrom 1.6020 to +1.5524 rad/sandfrom 0.1145 to +0.7598 rad, respectively. The 
attractive form of the - is known as strange attractor (chaotic attractor).The strange 
attractorsof the LagainstVLare shown in Fig.11. The strange attractor coordinateswere from 
0.0345to 0.2748 rad and from 0.8285 to 1.1118pu for Lmax- Lmin and VLmax-VLmin, respectively. 



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Meanwhile, the RNN model of the L-VLwas from 0.0332to 0.2618 rad and from 0.8280 to 
1.1235pu for Lmax- Lmin and VLmax-VLmin, respectively.  
 

Table4.Power system state when variation of the DE was applied. 
0&Model (rad) (rad/s) L (rad/s) VL (pu) 

0.5Exact eq 0.3095 osc 0.2104 to 
0.2123 

eq 
0.1128 

eq 1.095 

RNN eq 0.3194 osc 0.2008 to 
0.2010 

eq 
0.1116 

eq 1.008 

MSE  (%) 0.2636 11.1792 3.8193 8.7051 
1.3824Exact osc 0.0245 

to 0.6160 
osc 1.1546 to 

1.1049 
osc0.0600 to 

0.1995 
osc0.9967 to 

1.1207 
RNN osc 0.0256 

to 0.6165 
osc 1.0246 to 

1.0049 
osc0.0501 to 

0.1879 
osc0.9970 to 

1.1135 
MSE (%) 3.9625 6.3023 0.2040 0.1154 
1.3425Exact osc 0.1156 

to 0.7578 
osc 1.5711 to 

1.5142 
osc0.0351 to 

0.2730 
osc0.8307 to 

1.1220 
RNN osc 0.1148 

to 0.7510 
osc 1.5734 to 

1.5165 
osc0.0460 to 

0.2644 
osc0.8497 to 

1.1158 
MSE  (%) 0.68 0.23 1.09 1.90 
1.6000Exact osc 0.1165 

to 0.7583 
osc 1.6011 to 

1.5535 
osc 0. 0345 
to 0. 2748 

osc 0.8285 to 
1. 1118 

RNN osc 0.1645 
to 0.7598 

osc 1.6020 to 
1.5524 

osc0.0332 to 
0. 2618 

osc0.8580 to 
1. 1235 

MSE(%) 0.2163 2.8779 0.0460 0.0407 
1.7003Exact osc .1157 to 

0.7601 
osc 1.6052 to 

1.5679 
osc 0. 0340 
to 0. 2756 

osc 0.8290 to 
1. 1119 

RNN osc 0.1345 
to 0.7457 

osc 1.511 to 
1.6045 

osc 0.0342 to 
0. 2613 

osc 0.8642 to 
1. 1185 

MSE(%) 1.0522 17.8296 0.1284 0.1470 
Note: eq = equilibrium point (fixed point); osc = oscillation. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
Figure 10. State trajectory of the -  when disturbance was applied at 0 = 1.600 

rad/s 
  



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Furthermore, existence of the chaotic attractors can also be depicted in Figs.12 and 13 for the 
01.7003 rad/s.  Fig.12 was produced by the againsts state trajectories at coordinates from 
1.6052 to +1.5679 rad/sandfrom 0.1157 to +0.7601 rad for the min- max and min- max, 

respectively. The results of theRNN model are depicted by red circles at coordinates from 
1.5110 to +1.6045 rad/sandfrom 0.1345 to +0.7457 rad for the min- max and min- max, 

respectively. 
 
Fig.13 shows the LagainstVL state trajectories at coordinates from 0.0351to 0.2756 rad and from 
0.8290 to 1.1119 pu for the Lmax- Lmin and the VLmax-VLmin, respectively. State trajectories of the 
RNN model can be depicted by red points at coordinates from 0.0342to 0.2613 rad and from 
0.8642 to 1.1185 pu for the Lmax- Lmin and the VLmax-VLmin, respectively. The complete simulation 
results are tabulated in Table 4. 
 

 
 

Figure 11. The L-VL state trajectory when the DE at 0 = 1.6 rad/s was applied 
 

 
Figure 12. The - state trajectory  when the DE at the value of 1.7003 rad/s was 

applied to a power system 
 



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Figure 13. The L-VLstate trajectory when the DE at the value of 1.7003 rad/s was applied 

to a power system 
 

Based on the in Table4that the largest MSE was 17.8296, where the largest MSE was obtained 
onthe speed rotor deviation ( ) at the value of 1.7003 rad/s. Simulation results show that 
chaotic behavior of power systems can be modeled by the Elman recurrent neural network. 
 
6. Conclusion 
 
Chaotic oscillationsin power systems using exact and RNN models are deeply studied in this 
research. The exact model was obtained using mathematical model. Then, the RNN model is 
obtained by training process using the data from exact model simulation. The training of the 
RNN model using adaptive learning rate both with and without momentum is compared. The 
performace of the adaptive learning rate with momentum is better than the other one. Chaotic 
behaviors are detected in power systems by appearing chaotic attractors both at power angle-
rotor speed and at magnitude-angle voltage state trajectories in phase-plane. 
 
7. Future Works 
 
Chaotic behavior of power systems was an interest topic research in recent years. In the future, 
thechaotic behavior of power systems should be reduced and vanished by applying control 
strategy properly. 
 
 
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