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Optimal Load Dispatch Using Ant Lion Optimization
Menakshi Mahendru Nischal1
, Shivani Mehta2
M.Tech student, DAVIET, Jalandhar1
Assistant Professor, DAVIET, Jalandhar2
Abstract
This paper presents Ant lion optimization (ALO) technique to solve optimal load dispatch problem. Ant lion
optimization (ALO) is a novel nature inspired algorithm. The ALO algorithm mimics the hunting mechanism of
ant lions in nature. Five main steps of hunting prey such as the random walk of ants, building traps, entrapment of
ants in traps, catching preys, and re-building traps are implemented. Optimal load dispatch (OLD) is a method of
determining the most efficient, low-cost and reliable operation of a power system by dispatching available
electricity generation resources to supply load on the system. The primary objective of OLD is to minimize total
cost of generation while honoring operational constraints of available generation resources. The proposed
technique is implemented on 3, 6 & 20 unit test system for solving the OLD. Numerical results shows that the
proposed method has good convergence property and better in quality of solution than other algorithms reported
in recent literature.
Keywords—ALO; Optimal load dispatch; transmission loss
Nomenclature:
ai, bi, ci : fuel cost coefficient of ith
generator,
Rs/MW2
h, Rs/MW h, Rs/h
F(Pg ) : total fuel cost, Rs/h
n : number of generators
𝑃𝑔𝑖
𝑚𝑖𝑛
: Minimum generation limit of ith
generator,
MW
𝑃𝑔𝑖
𝑚𝑎𝑥
: Maximum generation limit of ith
generator,
MW
Pl : Transmission losses, MW
Pd : Power demand, MW
I. INTRODUCTION
The operating cost of a power plant mainly
depends on the fuel cost of generators and is
minimized via optimal load dispatch. Optimal load
dispatch(OLD) problem can be defined as
determining the least cost power generation schedule
from a set of on line generating units to meet the total
power demand at a given point of time [1]. The main
objective of OLD problem is to decrease fuel cost of
generators, while satisfying equality and inequality
constraints. In this problem, fuel cost of generation is
represented as cost curves and overall calculation
minimizes the operating cost by finding a point
where total output of generators equals total power
that must be delivered plus losses.
In conventional optimal load dispatch, cost function
for each generator has been approximately
represented by a single quadratic function and is
solved using lambda iteration method, gradient-based
method,dynamic programming etc. [1]. Generally,
these approaches have hitches in finding an overall
optimum, usually offering local optimum point only.
Furthermore, traditional approaches require
calculating derivatives and certain inspection on
derivability and continuity conditions of function
belonging to optimization model. To overcome these
shortcomings quite a lot of nature based optimization
techniques were applied. Particle swarm optimization
[2] is one of the famous meta-heuristics applied to
solve OLD problem. Other approaches used for
solving OLD problems are: evolutionary
programming (EPs) [3], tabu search and multiple
tabu search (TS, MTS) [4], differential evolution
(DE) [5,6], hybrid DE (DEPSO) [7], artificial bee
colony algorithm (ABC) [8], simulated annealing
[9],biogeography-based optimization [10],genetic
algorithms [11], intelligent water drop algorithm[12]
,hybrid harmony search[13] , differential HS (DHS)
[14]gravitational search algorithm[15],firefly
algorithm[16],hybrid gravitational search[17],cuckoo
search (CS) [18],.have been successfully applied to
OLD problems.
II. PROBLEM FORMULATION
The objective function of the OLD problem is to
minimize the total generation cost while satisfying the
different constraints, when the necessary load demand
of a power system is being supplied. The objective
function to be minimized is given by the following
equation:
2
1
( ) ( )
n
g i gi i gi i
i
F P a P b P c

   … (1)
The total fuel cost has to be minimized with the
following constraints:
1) Power balance constraint
RESEARCH ARTICLE OPEN ACCESS
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ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19
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The total generation by all the generators must be
equal to the total power demand and system’s real
power loss.
𝑃𝑔𝑖 − 𝑃𝑑 − 𝑃𝑙
𝑛
𝑖=1 ….. (2)
2) Generator limit constraint
The real power generation of each generator is to
be controlled within its particular lower and upper
operating limits.
𝑃𝑔𝑖
𝑚𝑖𝑛
≤ 𝑃𝑔𝑖 ≤ 𝑃𝑔𝑖
𝑚𝑎𝑥
I =1,2,...,ng …..(3)
III. ANT LION OPTIMIZATION
Ant Lion Optimizer (ALO)[22] is a novel nature-
inspired algorithm proposed by SeyedaliMirjalili in
2015.The ALO algorithm mimics the hunting
mechanism of ant lions in nature. Five main steps of
hunting prey such as the random walk of ants,
building traps, entrapment of ants in traps, catching
preys, and re-building traps are implemented.
Ant lions (doodlebugs) belong to class of net
winged insects. The lifecycle of ant lions includes
two main phases: larvae and adult. A natural total
lifespan can take up to 3 years, which mostly occurs
in larvae (only 3–5 weeks for adulthood). Ant lions
undergo metamorphosis in a cocoon to become adult.
They mostly hunt in larvae and the adulthood period
is for reproduction. An ant lion larvae digs a cone-
shaped pit in sand by moving along a circular path
and throwing out sands with its massive jaw.After
digging the trap, the larvae hides underneath the
bottom of the cone and waits for insects (preferably
ant) to be trapped in the pit. The edge of the cone is
sharp enough for insects to fall to the bottom of the
trap easily.
Once the ant lion realizes that a prey is in the
trap, it tries to catch it.
Fig. 1. Cone-shaped traps and hunting behavior of ant lions[22]
Random walks of ants:Random walks are all based on the Eq.4
𝑋 𝑡 = 0, 𝑐𝑢𝑚𝑠𝑢𝑚 2𝑟 𝑡1 − 1 , 𝑐𝑢𝑚𝑠𝑢𝑚 2𝑟 𝑡2 − 1 , … … . . , 𝑐𝑢𝑚𝑠𝑢𝑚(2𝑟 𝑡 𝑛 − 1) ……(4)
Where cumsum calculates the cumulative sum, n is
the maximum number of iteration, t shows the step of
random walk and r(t) is a stochastic function defined
as follows:
𝑟 𝑡 =
1 𝑖𝑓 𝑟𝑎𝑛𝑑 > 0.5
0 𝑖𝑓 𝑟𝑎𝑛𝑑 ≤ 0.5
……(5)
however, above Eq. cannot be directly used for
updating position of ants. In order to keep the random
walks inside the search space, they are normalized
using the following equation (min–max
normalization):
𝑋𝑖
𝑡
=
(𝑋𝑖
𝑡
−𝑎 𝑖)×(𝑑 𝑖−𝑐 𝑖
𝑡
)
(𝑑 𝑖
𝑡
−𝑎 𝑖)
+ 𝑐𝑖 ……(6)
Where ai is the minimum of random walk of ith
variable, bi is the maximum of random walk in ith
variable, 𝑐𝑖
𝑡
is the minimum of ith
variable at tth
iteration, and 𝑑𝑖
𝑡
indicates the maximum of ith
variable
at tth
iteration
Trapping in ant lion's pits: random walks of ants
are affected by antlions’ traps. In order to
mathematically model this assumption, the following
equations are proposed:
𝐶𝑖
𝑡
= 𝐴𝑛𝑡𝑙𝑖𝑜𝑛𝑗
𝑡
+ 𝐶 𝑡
….(7)
𝑑𝑖
𝑡
= 𝐴𝑛𝑡𝑙𝑖𝑜𝑛𝑗
𝑡
+ …(8)
where 𝐶 𝑡
is the minimum of all variables at tth
iteration, 𝑑 𝑡
indicates the vector including the
maximum of all variables at tth
iteration, 𝐶𝑗
𝑡
is the
minimum of all variables for ith
ant, 𝑑𝑗
𝑡
is the
maximum of all variables for ith
ant, and Antliont j
shows the position of the selected j-thantlion at
tth
iteration
Building trap:In order to model the ant-lions’s
hunting capability, a roulette wheel is employed. The
ALO algorithm is required to utilize a roulette wheel
operator for selecting ant lions based of their fitness
M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com
ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19
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during optimization. This mechanism gives high
chances to the fitter ant lions for catching ants.
Sliding ants towards ant lion:With the mechanisms
proposed so far, ant lions are able to build traps
proportional to their fitness and ants are required to
move randomly. However, ant lions shoot sands
outwards the center of the pit once they realize that
an ant is in the trap. This behavior slides down the
trapped ant that is trying to escape. For
mathematically modelling this behavior, the radius of
ants' random walks hyper-sphere is decreased
adaptively. The following equations are proposed in
this regard:
𝐶 𝑡
=
…(9)
𝑑 𝑡
=
…(10)
where I is a ratio, ct is the minimum of all variables
at t-th iteration, and dt indicates the vector including
the maximum of all variables at t-th iteration.
Catching prey and re-building the pit:The final
stage of hunt is when an ant reaches the bottom of the
pit and is caught in the antlion’s jaw. After this stage,
the antlion pulls the ant inside the sand and consumes
its body. For mimicking this process, it is assumed
that catching prey occur when ants becomes fitter
(goes inside sand) than its corresponding antlion. An
antlion is then required to update its position to the
latest position of the hunted ant to enhance its chance
of catching new prey. The following equation is
proposed in this regard:
𝐴𝑛𝑡𝑙𝑖𝑜𝑛𝑗
𝑡
= 𝐴𝑛𝑡𝑖
𝑡
𝑖𝑓 𝑓 𝐴𝑛𝑡𝑖
𝑡
> 𝑓 …(11)
where t shows the current iteration, Antliont j shows
the position of selected j-thantlion at t-th iteration,
and Antti indicates the position of i-th ant at t-th
iteration.
Elitism: Elitism is an important characteristic of
evolutionary algorithms that allows them to maintain
the best solution(s) obtained at any stage of
optimization process. Since the elite is the fittest
antlion, it should be able to affect the movements of
all the ants during iterations. Therefore, it is assumed
that every ant randomly walks around a selected
antlion by the roulette wheel and the elite
simultaneously as follows:
𝐴𝑛𝑡𝑖
𝑡
=
𝑅 𝐴
𝑡
+𝑅 𝐸
𝑡
2
… (12)
where 𝑅 𝐴
𝑡
is the random walk around the antlion
selected by the roulette wheel at t-th iteration, 𝑅 𝐸
𝑡
is
the random walk around the elite at t-th iteration, and
𝐴𝑛𝑡𝑖
𝑡
indicates the position of i-th ant at t-th iteration
IV. RESULTS & DISCUSSIONS
ALO has been used to solve the OLD problems
in three different test cases for exploring its
optimization potential, where the objective function
was limited within power ranges of the generating
units and transmission losses were also taken into
account. The iterations performed for each test case
are 500 and number of search agents (population)
taken in both test cases is 30.
1) Test system I: Three generating units
The input data for three generators and loss
coefficient matrix Bmn is derived from reference [19]
and is given in table 4.1.
Table 4.1: Generating unit data for test case I
Unit ai bi ci 𝑷 𝒈𝒊
𝒎𝒊𝒏 𝑷 𝒈𝒊
𝒎𝒂𝒙
1 0.03546 38.30553 1243.531
1
35 210
2 0.02111 36.32782 1658.569
6
130 325
3 0.01799 38.27041 1356.659
2
125 315
Bmn=
0.000071 0.000030 0.000025
0.000030 0.000069 0.000032
0.000025 0.000032 0.000080
Table 4.1: Optimal load dispatch for 3 unit system
Without Loss With Loss
Power Demand
(MW)
400 500 600 400 500 600
P1 75.724 97.225 118.73 82.078 105.88 130.02
P2 174.04 210.16 246.28 174.99 212.73 250.85
P3 150.23 192.62 235 150.5 193.31 236.44
Power loss - - - 7.568125 11.91438 17.30402
Cost(Rs/hr)
20480.29
695
24924.12631 29520.44334 20812.2936 25465.4691 30333.9858
Table 4.2: Power loss comparison
Sr. no. Power demand Power losses
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FFA[19] ALO
1 400 7.56813 7.568125
2 500 11.9144 11.91438
3 600 17.3040 17.30402
Table 4.3: Fuel cost comparison with other methods
Sr.no. Power demand
(MW)
Fuel Cost (Rs/hr)
Lambda
iteration[19]
FFA[19] ALO
1 400 20817.4 20812.3 20812.2936
2 500 25495.2 25465.5 25465.46914
3 600 30359.3 30334.0 30333.9858
Fig 4.1. Fuel cost with and without losses for 3 unit system
0
5000
10000
15000
20000
25000
30000
35000
400 500 600
CostRs/hr
Power Demand
without loss
with loss
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Fig 4.2. Fuel cost comparison for 3 unit system
2) Test system II: Six generating units
The input data for six generators and loss coefficient matrix Bmn is derived from reference [19] and is given
in table 4.4.
Table 4.4: Generating unit data for test case II
Unit ai bi ci 𝑷 𝒈𝒊
𝒎𝒊𝒏 𝑷 𝒈𝒊
𝒎𝒂𝒙
1 0.15240 38.53973 756.79886 10 125
2 0.10587 46.15916 451.32513 10 150
3 0.02803 40.39655 1049.9977 35 225
4 0.03546 38.30553 1243.5311 35 210
5 0.02111 36.32782 1658.5596 130 325
6 0.01799 38.27041 1356.6592 125 315
Bmn=
0.000014 0.000017 0.000015 0.000019 0.000026 0.000022
0.000017 0.000060 0.000013 0.000016 0.000015 0.000020
0.000015 0.000013 0.000065 0.000017 0.000024 0.000019
0.000019 0.000016 0.000017 0.000072 0.000030 0.000025
0.000026 0.000015 0.000024 0.000030 0.000069 0.000032
0.000022 0.000020 0.000019 0.000025 0.000032 0.000085
Table 4.5: Optimal load dispatch for 6 unit system
Without Loss With Loss
Power Demand
(MW)
600 700 800 600 700 800
P1 21.19 24.974 28.758 23.8713 28.3031 32.6003
P2 10 10 10 10 10.00 14.4830
P3 82.086 102.66 123.24 95.6365 118.9550 141.5440
P4 94.371 110.63 126.9 100.7064 118.6728 136.0413
P5 205.36 232.68 260 202.8285 230.7596 257.6587
P6 186.99 219.05 251.1 181.1945 212.7411 243.0033
Power loss - - - 14.2372 19.4317 25.3307
Cost(Rs/hr) 31445.62289 36003.12394 40675.96798 32094.6783 36912.1444 41896.6286
30320
30325
30330
30335
30340
30345
30350
30355
30360
30365
CostRs/hr
Power Demand= 600 MW
Lambda iteration
FFA
ALO
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Fig 4.3 fuel cost for 6 unit with and without loss
Table 4.6: comparison of power losses.
Sr. no. Power demand
Power losses
Conventional[2] PSO[2] FFA[19] ALO
1 600 15.07 14.2374 14.2374 14.2372
2 700 19.50 19.4319 19.4319 19.4317
3 800 25.34 25.3309 25.3312 25.3307
Table 4.7: Comparison of fuel cost with other methods
Sr.no. Power
demand
(MW)
Fuel Cost (Rs/hr)
Conventional
Method[2]
PSO[2] Lambda
iteration[19]
FFA[19] ALO
1 600 32096.58 32094.69 32129.8 32094.7 32094.6783
2 700 36914.01 36912.16 36946.4 36912.2 36912.1444
3 800 41898.45 41896.66 41959.0 41896.9 41896.6286
25000
27000
29000
31000
33000
35000
37000
39000
41000
43000
600 700 800
CostRs/hr
POWER DEMAND
without loss
with loss
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Fig 4.4. Fuel cost comparison for 6 unit system
3) Test system III: Twenty generating units
The input data for six generators and loss coefficient matrix Bmn is derived from reference [20] and is
given in table 4.8.
Table 4.8: generating data for 20 units
Unit ai($/MW2) bi ($/MW) ci ($) 𝑷 𝒈𝒊
𝒎𝒊𝒏 𝑷 𝒈𝒊
𝒎𝒂𝒙
1 0.00068 18.19 1000 150 600
2 0.00071 19.26 970 50 200
3 0.00650 19.80 600 50 200
4 0.00500 19.10 700 50 200
5 0.00738 18.10 420 50 160
6 0.00612 19.26 360 20 100
7 0.00790 17.14 490 25 125
8 0.00813 18.92 660 50 150
9 0.00522 18.27 765 50 200
10 0.00573 18.92 770 30 150
11 0.00480 16.69 800 100 300
12 0.00310 16.76 970 150 500
13 0.00850 17.36 900 40 160
14 0.00511 18.70 700 20 130
15 0.00398 18.70 450 25 185
16 0.07120 14.26 370 20 80
17 0.00890 19.14 480 30 85
18 0.00713 18.92 680 30 120
19 0.00622 18.47 700 40 120
20 0.00773 19.79 850 30 100
41860
41870
41880
41890
41900
41910
41920
41930
41940
41950
41960
41970
Power Demand = 800 MW
Conventional Method
PSO
Lambda Iteration
FFA
ALO
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Table 4.9: optimal load dispatch for 20-generating units without loss (PD = 2500 MW)
Unit ALO
P1 600
P2 172.85
P3 50
P4 50.481
P5 95.285
P6 24.17
P7 124.81
P8 50
P9 91.891
P10 44.961
P11 275.5
P12 427.35
P13 123.15
P14 59.795
P15 101.7
P16 36.26
P17 36.342
P18 34.196
P19 71.267
P20 30
Total generation (MW) 2500.00
Total generation cost ($/h) 60160.71425
Table 4.10: optimal load dispatch for 20-generating units withloss (PD = 2500 MW)
Unit BBO [21] LI [20] HM [20] ALO
P1 513.0892 512.7805 512.7804 512.78
P2 173.3533 169.1033 169.1035 169.11
P3 126.9231 126.8898 126.8897 126.89
P4 103.3292 102.8657 102.8656 102.87
P5 113.7741 113.6386 113.6836 113.68
P6 73.06694 73.5710 73.5709 73.568
P7 114.9843 115.2878 115.2876 115.29
P8 116.4238 116.3994 116.3994 116.4
P9 100.6948 100.4062 100.4063 100.41
P10 99.99979 106.0267 106.0267 106.02
P11 148.9770 150.2394 150.2395 150.24
P12 294.0207 292.7648 292.7647 292.77
P13 119.5754 119.1154 119.1155 119.12
P14 30.54786 30.8340 30.8342 30.831
P15 116.4546 115.8057 115.8056 115.81
P16 36.22787 36.2545 36.2545 36.254
P17 66.85943 66.8590 66.8590 66.857
P18 88.54701 87.9720 87.9720 87.975
P19 100.9802 100.8033 100.8033 100.8
P20 54.2725 54.3050 54.3050 54.305
Total generation (MW) 2592.1011 2591.9670 2591.9670 2591.967
Total transmission loss (MW) 92.1011 91.9670 91.9669 91.9662
Total generation cost ($/h) 62456.77926 62456.6391 62456.6341 62456.63309
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V. CONCLUSION
In this paper optimal load dispatch problem has
been solved by using ALO. The results of ALO are
compared for three ,six and twenty generating unit
systems with other techniques. The algorithm is
programmed in MATLAB(R2009b) software
package. The results displayefficacy of ALO
algorithm for solving the optimal load dispatch
problem. The advantage of ALO algorithm is its
simplicity, reliability and efficiency for practical
applications.
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62456.55
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M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com
ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19
www.ijera.com 19 | P a g e
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Optimal Load Dispatch Using Ant Lion Optimization

  • 1. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 10 | P a g e Optimal Load Dispatch Using Ant Lion Optimization Menakshi Mahendru Nischal1 , Shivani Mehta2 M.Tech student, DAVIET, Jalandhar1 Assistant Professor, DAVIET, Jalandhar2 Abstract This paper presents Ant lion optimization (ALO) technique to solve optimal load dispatch problem. Ant lion optimization (ALO) is a novel nature inspired algorithm. The ALO algorithm mimics the hunting mechanism of ant lions in nature. Five main steps of hunting prey such as the random walk of ants, building traps, entrapment of ants in traps, catching preys, and re-building traps are implemented. Optimal load dispatch (OLD) is a method of determining the most efficient, low-cost and reliable operation of a power system by dispatching available electricity generation resources to supply load on the system. The primary objective of OLD is to minimize total cost of generation while honoring operational constraints of available generation resources. The proposed technique is implemented on 3, 6 & 20 unit test system for solving the OLD. Numerical results shows that the proposed method has good convergence property and better in quality of solution than other algorithms reported in recent literature. Keywords—ALO; Optimal load dispatch; transmission loss Nomenclature: ai, bi, ci : fuel cost coefficient of ith generator, Rs/MW2 h, Rs/MW h, Rs/h F(Pg ) : total fuel cost, Rs/h n : number of generators 𝑃𝑔𝑖 𝑚𝑖𝑛 : Minimum generation limit of ith generator, MW 𝑃𝑔𝑖 𝑚𝑎𝑥 : Maximum generation limit of ith generator, MW Pl : Transmission losses, MW Pd : Power demand, MW I. INTRODUCTION The operating cost of a power plant mainly depends on the fuel cost of generators and is minimized via optimal load dispatch. Optimal load dispatch(OLD) problem can be defined as determining the least cost power generation schedule from a set of on line generating units to meet the total power demand at a given point of time [1]. The main objective of OLD problem is to decrease fuel cost of generators, while satisfying equality and inequality constraints. In this problem, fuel cost of generation is represented as cost curves and overall calculation minimizes the operating cost by finding a point where total output of generators equals total power that must be delivered plus losses. In conventional optimal load dispatch, cost function for each generator has been approximately represented by a single quadratic function and is solved using lambda iteration method, gradient-based method,dynamic programming etc. [1]. Generally, these approaches have hitches in finding an overall optimum, usually offering local optimum point only. Furthermore, traditional approaches require calculating derivatives and certain inspection on derivability and continuity conditions of function belonging to optimization model. To overcome these shortcomings quite a lot of nature based optimization techniques were applied. Particle swarm optimization [2] is one of the famous meta-heuristics applied to solve OLD problem. Other approaches used for solving OLD problems are: evolutionary programming (EPs) [3], tabu search and multiple tabu search (TS, MTS) [4], differential evolution (DE) [5,6], hybrid DE (DEPSO) [7], artificial bee colony algorithm (ABC) [8], simulated annealing [9],biogeography-based optimization [10],genetic algorithms [11], intelligent water drop algorithm[12] ,hybrid harmony search[13] , differential HS (DHS) [14]gravitational search algorithm[15],firefly algorithm[16],hybrid gravitational search[17],cuckoo search (CS) [18],.have been successfully applied to OLD problems. II. PROBLEM FORMULATION The objective function of the OLD problem is to minimize the total generation cost while satisfying the different constraints, when the necessary load demand of a power system is being supplied. The objective function to be minimized is given by the following equation: 2 1 ( ) ( ) n g i gi i gi i i F P a P b P c     … (1) The total fuel cost has to be minimized with the following constraints: 1) Power balance constraint RESEARCH ARTICLE OPEN ACCESS
  • 2. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 11 | P a g e The total generation by all the generators must be equal to the total power demand and system’s real power loss. 𝑃𝑔𝑖 − 𝑃𝑑 − 𝑃𝑙 𝑛 𝑖=1 ….. (2) 2) Generator limit constraint The real power generation of each generator is to be controlled within its particular lower and upper operating limits. 𝑃𝑔𝑖 𝑚𝑖𝑛 ≤ 𝑃𝑔𝑖 ≤ 𝑃𝑔𝑖 𝑚𝑎𝑥 I =1,2,...,ng …..(3) III. ANT LION OPTIMIZATION Ant Lion Optimizer (ALO)[22] is a novel nature- inspired algorithm proposed by SeyedaliMirjalili in 2015.The ALO algorithm mimics the hunting mechanism of ant lions in nature. Five main steps of hunting prey such as the random walk of ants, building traps, entrapment of ants in traps, catching preys, and re-building traps are implemented. Ant lions (doodlebugs) belong to class of net winged insects. The lifecycle of ant lions includes two main phases: larvae and adult. A natural total lifespan can take up to 3 years, which mostly occurs in larvae (only 3–5 weeks for adulthood). Ant lions undergo metamorphosis in a cocoon to become adult. They mostly hunt in larvae and the adulthood period is for reproduction. An ant lion larvae digs a cone- shaped pit in sand by moving along a circular path and throwing out sands with its massive jaw.After digging the trap, the larvae hides underneath the bottom of the cone and waits for insects (preferably ant) to be trapped in the pit. The edge of the cone is sharp enough for insects to fall to the bottom of the trap easily. Once the ant lion realizes that a prey is in the trap, it tries to catch it. Fig. 1. Cone-shaped traps and hunting behavior of ant lions[22] Random walks of ants:Random walks are all based on the Eq.4 𝑋 𝑡 = 0, 𝑐𝑢𝑚𝑠𝑢𝑚 2𝑟 𝑡1 − 1 , 𝑐𝑢𝑚𝑠𝑢𝑚 2𝑟 𝑡2 − 1 , … … . . , 𝑐𝑢𝑚𝑠𝑢𝑚(2𝑟 𝑡 𝑛 − 1) ……(4) Where cumsum calculates the cumulative sum, n is the maximum number of iteration, t shows the step of random walk and r(t) is a stochastic function defined as follows: 𝑟 𝑡 = 1 𝑖𝑓 𝑟𝑎𝑛𝑑 > 0.5 0 𝑖𝑓 𝑟𝑎𝑛𝑑 ≤ 0.5 ……(5) however, above Eq. cannot be directly used for updating position of ants. In order to keep the random walks inside the search space, they are normalized using the following equation (min–max normalization): 𝑋𝑖 𝑡 = (𝑋𝑖 𝑡 −𝑎 𝑖)×(𝑑 𝑖−𝑐 𝑖 𝑡 ) (𝑑 𝑖 𝑡 −𝑎 𝑖) + 𝑐𝑖 ……(6) Where ai is the minimum of random walk of ith variable, bi is the maximum of random walk in ith variable, 𝑐𝑖 𝑡 is the minimum of ith variable at tth iteration, and 𝑑𝑖 𝑡 indicates the maximum of ith variable at tth iteration Trapping in ant lion's pits: random walks of ants are affected by antlions’ traps. In order to mathematically model this assumption, the following equations are proposed: 𝐶𝑖 𝑡 = 𝐴𝑛𝑡𝑙𝑖𝑜𝑛𝑗 𝑡 + 𝐶 𝑡 ….(7) 𝑑𝑖 𝑡 = 𝐴𝑛𝑡𝑙𝑖𝑜𝑛𝑗 𝑡 + …(8) where 𝐶 𝑡 is the minimum of all variables at tth iteration, 𝑑 𝑡 indicates the vector including the maximum of all variables at tth iteration, 𝐶𝑗 𝑡 is the minimum of all variables for ith ant, 𝑑𝑗 𝑡 is the maximum of all variables for ith ant, and Antliont j shows the position of the selected j-thantlion at tth iteration Building trap:In order to model the ant-lions’s hunting capability, a roulette wheel is employed. The ALO algorithm is required to utilize a roulette wheel operator for selecting ant lions based of their fitness
  • 3. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 12 | P a g e during optimization. This mechanism gives high chances to the fitter ant lions for catching ants. Sliding ants towards ant lion:With the mechanisms proposed so far, ant lions are able to build traps proportional to their fitness and ants are required to move randomly. However, ant lions shoot sands outwards the center of the pit once they realize that an ant is in the trap. This behavior slides down the trapped ant that is trying to escape. For mathematically modelling this behavior, the radius of ants' random walks hyper-sphere is decreased adaptively. The following equations are proposed in this regard: 𝐶 𝑡 = …(9) 𝑑 𝑡 = …(10) where I is a ratio, ct is the minimum of all variables at t-th iteration, and dt indicates the vector including the maximum of all variables at t-th iteration. Catching prey and re-building the pit:The final stage of hunt is when an ant reaches the bottom of the pit and is caught in the antlion’s jaw. After this stage, the antlion pulls the ant inside the sand and consumes its body. For mimicking this process, it is assumed that catching prey occur when ants becomes fitter (goes inside sand) than its corresponding antlion. An antlion is then required to update its position to the latest position of the hunted ant to enhance its chance of catching new prey. The following equation is proposed in this regard: 𝐴𝑛𝑡𝑙𝑖𝑜𝑛𝑗 𝑡 = 𝐴𝑛𝑡𝑖 𝑡 𝑖𝑓 𝑓 𝐴𝑛𝑡𝑖 𝑡 > 𝑓 …(11) where t shows the current iteration, Antliont j shows the position of selected j-thantlion at t-th iteration, and Antti indicates the position of i-th ant at t-th iteration. Elitism: Elitism is an important characteristic of evolutionary algorithms that allows them to maintain the best solution(s) obtained at any stage of optimization process. Since the elite is the fittest antlion, it should be able to affect the movements of all the ants during iterations. Therefore, it is assumed that every ant randomly walks around a selected antlion by the roulette wheel and the elite simultaneously as follows: 𝐴𝑛𝑡𝑖 𝑡 = 𝑅 𝐴 𝑡 +𝑅 𝐸 𝑡 2 … (12) where 𝑅 𝐴 𝑡 is the random walk around the antlion selected by the roulette wheel at t-th iteration, 𝑅 𝐸 𝑡 is the random walk around the elite at t-th iteration, and 𝐴𝑛𝑡𝑖 𝑡 indicates the position of i-th ant at t-th iteration IV. RESULTS & DISCUSSIONS ALO has been used to solve the OLD problems in three different test cases for exploring its optimization potential, where the objective function was limited within power ranges of the generating units and transmission losses were also taken into account. The iterations performed for each test case are 500 and number of search agents (population) taken in both test cases is 30. 1) Test system I: Three generating units The input data for three generators and loss coefficient matrix Bmn is derived from reference [19] and is given in table 4.1. Table 4.1: Generating unit data for test case I Unit ai bi ci 𝑷 𝒈𝒊 𝒎𝒊𝒏 𝑷 𝒈𝒊 𝒎𝒂𝒙 1 0.03546 38.30553 1243.531 1 35 210 2 0.02111 36.32782 1658.569 6 130 325 3 0.01799 38.27041 1356.659 2 125 315 Bmn= 0.000071 0.000030 0.000025 0.000030 0.000069 0.000032 0.000025 0.000032 0.000080 Table 4.1: Optimal load dispatch for 3 unit system Without Loss With Loss Power Demand (MW) 400 500 600 400 500 600 P1 75.724 97.225 118.73 82.078 105.88 130.02 P2 174.04 210.16 246.28 174.99 212.73 250.85 P3 150.23 192.62 235 150.5 193.31 236.44 Power loss - - - 7.568125 11.91438 17.30402 Cost(Rs/hr) 20480.29 695 24924.12631 29520.44334 20812.2936 25465.4691 30333.9858 Table 4.2: Power loss comparison Sr. no. Power demand Power losses
  • 4. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 13 | P a g e FFA[19] ALO 1 400 7.56813 7.568125 2 500 11.9144 11.91438 3 600 17.3040 17.30402 Table 4.3: Fuel cost comparison with other methods Sr.no. Power demand (MW) Fuel Cost (Rs/hr) Lambda iteration[19] FFA[19] ALO 1 400 20817.4 20812.3 20812.2936 2 500 25495.2 25465.5 25465.46914 3 600 30359.3 30334.0 30333.9858 Fig 4.1. Fuel cost with and without losses for 3 unit system 0 5000 10000 15000 20000 25000 30000 35000 400 500 600 CostRs/hr Power Demand without loss with loss
  • 5. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 14 | P a g e Fig 4.2. Fuel cost comparison for 3 unit system 2) Test system II: Six generating units The input data for six generators and loss coefficient matrix Bmn is derived from reference [19] and is given in table 4.4. Table 4.4: Generating unit data for test case II Unit ai bi ci 𝑷 𝒈𝒊 𝒎𝒊𝒏 𝑷 𝒈𝒊 𝒎𝒂𝒙 1 0.15240 38.53973 756.79886 10 125 2 0.10587 46.15916 451.32513 10 150 3 0.02803 40.39655 1049.9977 35 225 4 0.03546 38.30553 1243.5311 35 210 5 0.02111 36.32782 1658.5596 130 325 6 0.01799 38.27041 1356.6592 125 315 Bmn= 0.000014 0.000017 0.000015 0.000019 0.000026 0.000022 0.000017 0.000060 0.000013 0.000016 0.000015 0.000020 0.000015 0.000013 0.000065 0.000017 0.000024 0.000019 0.000019 0.000016 0.000017 0.000072 0.000030 0.000025 0.000026 0.000015 0.000024 0.000030 0.000069 0.000032 0.000022 0.000020 0.000019 0.000025 0.000032 0.000085 Table 4.5: Optimal load dispatch for 6 unit system Without Loss With Loss Power Demand (MW) 600 700 800 600 700 800 P1 21.19 24.974 28.758 23.8713 28.3031 32.6003 P2 10 10 10 10 10.00 14.4830 P3 82.086 102.66 123.24 95.6365 118.9550 141.5440 P4 94.371 110.63 126.9 100.7064 118.6728 136.0413 P5 205.36 232.68 260 202.8285 230.7596 257.6587 P6 186.99 219.05 251.1 181.1945 212.7411 243.0033 Power loss - - - 14.2372 19.4317 25.3307 Cost(Rs/hr) 31445.62289 36003.12394 40675.96798 32094.6783 36912.1444 41896.6286 30320 30325 30330 30335 30340 30345 30350 30355 30360 30365 CostRs/hr Power Demand= 600 MW Lambda iteration FFA ALO
  • 6. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 15 | P a g e Fig 4.3 fuel cost for 6 unit with and without loss Table 4.6: comparison of power losses. Sr. no. Power demand Power losses Conventional[2] PSO[2] FFA[19] ALO 1 600 15.07 14.2374 14.2374 14.2372 2 700 19.50 19.4319 19.4319 19.4317 3 800 25.34 25.3309 25.3312 25.3307 Table 4.7: Comparison of fuel cost with other methods Sr.no. Power demand (MW) Fuel Cost (Rs/hr) Conventional Method[2] PSO[2] Lambda iteration[19] FFA[19] ALO 1 600 32096.58 32094.69 32129.8 32094.7 32094.6783 2 700 36914.01 36912.16 36946.4 36912.2 36912.1444 3 800 41898.45 41896.66 41959.0 41896.9 41896.6286 25000 27000 29000 31000 33000 35000 37000 39000 41000 43000 600 700 800 CostRs/hr POWER DEMAND without loss with loss
  • 7. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 16 | P a g e Fig 4.4. Fuel cost comparison for 6 unit system 3) Test system III: Twenty generating units The input data for six generators and loss coefficient matrix Bmn is derived from reference [20] and is given in table 4.8. Table 4.8: generating data for 20 units Unit ai($/MW2) bi ($/MW) ci ($) 𝑷 𝒈𝒊 𝒎𝒊𝒏 𝑷 𝒈𝒊 𝒎𝒂𝒙 1 0.00068 18.19 1000 150 600 2 0.00071 19.26 970 50 200 3 0.00650 19.80 600 50 200 4 0.00500 19.10 700 50 200 5 0.00738 18.10 420 50 160 6 0.00612 19.26 360 20 100 7 0.00790 17.14 490 25 125 8 0.00813 18.92 660 50 150 9 0.00522 18.27 765 50 200 10 0.00573 18.92 770 30 150 11 0.00480 16.69 800 100 300 12 0.00310 16.76 970 150 500 13 0.00850 17.36 900 40 160 14 0.00511 18.70 700 20 130 15 0.00398 18.70 450 25 185 16 0.07120 14.26 370 20 80 17 0.00890 19.14 480 30 85 18 0.00713 18.92 680 30 120 19 0.00622 18.47 700 40 120 20 0.00773 19.79 850 30 100 41860 41870 41880 41890 41900 41910 41920 41930 41940 41950 41960 41970 Power Demand = 800 MW Conventional Method PSO Lambda Iteration FFA ALO
  • 8. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 17 | P a g e Table 4.9: optimal load dispatch for 20-generating units without loss (PD = 2500 MW) Unit ALO P1 600 P2 172.85 P3 50 P4 50.481 P5 95.285 P6 24.17 P7 124.81 P8 50 P9 91.891 P10 44.961 P11 275.5 P12 427.35 P13 123.15 P14 59.795 P15 101.7 P16 36.26 P17 36.342 P18 34.196 P19 71.267 P20 30 Total generation (MW) 2500.00 Total generation cost ($/h) 60160.71425 Table 4.10: optimal load dispatch for 20-generating units withloss (PD = 2500 MW) Unit BBO [21] LI [20] HM [20] ALO P1 513.0892 512.7805 512.7804 512.78 P2 173.3533 169.1033 169.1035 169.11 P3 126.9231 126.8898 126.8897 126.89 P4 103.3292 102.8657 102.8656 102.87 P5 113.7741 113.6386 113.6836 113.68 P6 73.06694 73.5710 73.5709 73.568 P7 114.9843 115.2878 115.2876 115.29 P8 116.4238 116.3994 116.3994 116.4 P9 100.6948 100.4062 100.4063 100.41 P10 99.99979 106.0267 106.0267 106.02 P11 148.9770 150.2394 150.2395 150.24 P12 294.0207 292.7648 292.7647 292.77 P13 119.5754 119.1154 119.1155 119.12 P14 30.54786 30.8340 30.8342 30.831 P15 116.4546 115.8057 115.8056 115.81 P16 36.22787 36.2545 36.2545 36.254 P17 66.85943 66.8590 66.8590 66.857 P18 88.54701 87.9720 87.9720 87.975 P19 100.9802 100.8033 100.8033 100.8 P20 54.2725 54.3050 54.3050 54.305 Total generation (MW) 2592.1011 2591.9670 2591.9670 2591.967 Total transmission loss (MW) 92.1011 91.9670 91.9669 91.9662 Total generation cost ($/h) 62456.77926 62456.6391 62456.6341 62456.63309
  • 9. M Mahendru Nischal et al. Int. Journal of Engineering Research and Applications www.ijera.com ISSN: 2248-9622, Vol. 5, Issue 8, (Part - 2) August 2015, pp.10-19 www.ijera.com 18 | P a g e V. CONCLUSION In this paper optimal load dispatch problem has been solved by using ALO. The results of ALO are compared for three ,six and twenty generating unit systems with other techniques. The algorithm is programmed in MATLAB(R2009b) software package. The results displayefficacy of ALO algorithm for solving the optimal load dispatch problem. The advantage of ALO algorithm is its simplicity, reliability and efficiency for practical applications. References [1] A.J Wood and B.F. Wollenberg, Power Generation, Operation, and Control, John Wiley and Sons, New York, 1984. [2] Yohannes, M. S. "Solving optimal load dispatch problem using particle swarm optimization technique." International Journal of Intelligent Systems and Applications (IJISA) 4, no. 12 (2012): 12. [3] Sinha N., Chakrabarti R. and Chattopadhyay P.K., Evolutionary Programming Techniques for Optimal load dispatch, IEEE Transcations on Evolutionary Computation, 2003,20(1):83~94. [4] POTHIYA, S., I. NGAMROO, W. KONGPRAWECHNON, Application of Multiple Tabu Search Algorithm to Solve Dynamic Economic Dispatch Considering Generator Constraints, Energy Conversion and Management, Vol. 49(4), 2008, pp. 506- 516. [5] NOMAN, N., H. IBA, Differential Evolution for Optimal load dispatch Problems, Electric Power System Research, Vol. 78(3), 2008, pp. 1322-1331. 17. [6] PEREZ-GUERRERO, R. E. J. R. CEDENIO-MALDONADO, Economic Power Dispatch with Non-smooth Cost Functions using Differential Evolution, Proceedings of the 37th Annual North American, Power Symposium, Ames, Iowa, 2005, pp. 183-190. [7] SAYAH, S., A. HAMOUDA, A Hybrid Differential Evolution Algorithm based on Particle Swarm optimization for Non- convex Economic Dispatch Problems, Applied Soft Computing, Vol. 13(4), 2013, pp. 1608-1619. [8] HEMAMALINI, S., S. P. SIMON, Artificial Bee Colony Algorithm for Optimal load dispatch Problem with Non-smooth Cost Functions, Electric Power Components and Systems, Vol. 38(7), 2010, pp. 786-803. [9] Basu, M. "A simulated annealing-based goal-attainment method for economic emission load dispatch of fixed head hydrothermal power systems." International Journal of Electrical Power & Energy Systems 27, no. 2 (2005): 147-153. [10] Aniruddha Bhattacharya, P.K. Chattopadhyay, “Solving complex optimal load dispatch problems using biogeography- based optimization”, Expert Systems with Applications, Vol. 37, pp. 36053615, 2010. [11] Youssef, H. K., and El-Naggar, K. M., “Genetic based algorithm for security constrained power system economic 62456.55 62456.6 62456.65 62456.7 62456.75 62456.8 Cost$/hr Power demand = 2500 MW BBO LI HM ALO
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