A Novel Adaptive Ant Lion Optimizer for Global Numerical Optimization

DOI : 10.17577/IJERTV7IS020082

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A Novel Adaptive Ant Lion Optimizer for Global Numerical Optimization

Naveen Sihag1

Ph.D. Scholar Department of Computer Engineering, Rajasthan Technical University Kota,

Rajasthan 324002, India1

Abstract – A novel bio-inspired optimization algorithm based on the hunting process of Ant Lions in nature is known the Ant Lion optimizer (ALO) Algorithm in contrast to meta-heuristics; main feature is randomization having a relevant role in both exploration and exploitation in optimization problem. A novel randomization technique termed adaptive technique is integrated with ALO and exercised on unconstraint test benchmark function and localization of partial discharge in transformer like geometry. ALO algorithm has quality feature that it uses simple mathematical equation to update position of Ants towards targeted optimal solution over the end of maximum iteration limit. Integration of new randomization adaptive technique provides potential that AALO algorithm to attain global optimal solution and faster convergence with less parameter dependency. Adaptive ALO (AALO) solutions are evaluated and results shows its competitively better performance over standard ALO optimization algorithms.

Keywords: Meta-heuristic; Ant Lion optimizer; Adaptive technique; Global optimal; Hunting; Sensor Position.

  1. INTRODUCTION

    The ALO technique reflects the intellectual activities of antlions in hunting ants in environment. The ALO algorithm [1] inspired by hunting process and it is the interface between antlions and ants in the trap. To model such interfaces, ants have to travel over the exploration space, and antlions are permitted to pursuit them and become fitter using traps.

    In the meta-heuristic algorithms, randomization play a very important role in both exploration and exploitation where more strengthen randomization techniques are Markov chains, Levy flights and Gaussian or normal distribution and new technique is adaptive technique. So meta-heuristic algorithms on integrated with adaptive technique results in less computational time to reach optimum solution, local minima avoidance and faster convergence.

    In past, many optimization algorithms based on gradient search for solving linear and non-linear equation but in gradient search method value of objective function and constraint unstable and multiple peaks if problem having more than one local optimum.

    Population based ALO is a meta-heuristic optimization algorithm has an ability to avoid local optima and get global optimal solution that make it appropriate for practical applications without structural modifications in algorithm for solving different constrained or unconstraint optimization problems. ALO integrated with adaptive technique reduces the computational times for highly complex problems.

    Paper under literature review are: Adaptive Cuckoo Search Algorithm (ACSA) [2] [3], QGA [4], Acoustic Partial discharge (PD)

    [5] [6], HGAPSO [7], PSACO [8], HSABA [9], PBILKH [10], KH-QPSO [11], IFA-HS [12], HS/FA [13], CKH [14], HS/BA [15], HPSACO [16], CSKH [17], HS-CSS [18], PSOHS [19], DEKH [20], HS/CS [21], HSBBO [22], CSS-PSO [23] etc.

    Recently trend of optimization is to improve performance of meta-heuristic algorithms [24] by integrating with chaos theory, Levy flights strategy, Adaptive randomization technique, Evolutionary boundary handling scheme, and genetic operators like as crossover and mutation. Popular genetic operators used in KH [25] that can accelerate its global convergence speed. Evolutionary constraint handling scheme is used in Interior Search Algorithm (ISA) [26] that avoid upper and lower limits of variables.

    The remainder of this paper is organized as follows: The next Section describes the Ant Lion optimizer and its algebraic equations are given in Section 2. Section 3 includes description of Adaptive technique. Section 4 consists of simulation results of unconstrained benchmark test function, convergence curve and tables of results compared with source algorithm. In Section 5 PD localization by acoustic emission, in section 6 conclusion is drawn. Finally, acknowledgment gives regards detail and at the end, references are written.

  2. ANT-LION OPTIMIZER

    The ALO technique proposed by Seyedali Mirjalili that reflects the intellectual activities of antlions in hunting ants in environment. To model such interfaces, ants have to travel over the exploration space, and antlions are permitted to pursuit them and become fitter using traps [1].

      1. Operators of ALO algorithm

        As ants travel randomly in nature when searching for food, a random walk is selected for demonstrating ants movement and it is given by following equation:

        X(t)=[0, cumsum(2r(t_1)-1),cumsum(2r(t_2)-1),,cumsum(2r(t_n)-1)] (1)

        Where, cumsum computes the cumulative sum, n is the maximum no. of iteration, t is the step of random walk (iteration), and r(t)

        is a stochastic function defined as follows:

        0 rand 0.5

        r(t) 1 rand 0.5

        Where, t is the step of random walk and rand represents a random number created by uniform distribution in the interval of [0, 1]. The location of ants are kept and used during optimization in the given matrix:

        A11

        A12

        . . A1d

        A A . . A

        21 22 2d

        M Ant

        . . . . .

        . . . . .

        (2)

        An1

        An2 . .

        And

        Where: M Ant

        = the matrix for storing the location of every ants,

        Aij = the value for jth variable (dimension) of ith ant, n = the no.

        of ants and d = the total no. of variables.

        For calculating individual ant, a fitness function is used in optimisation and subsequent matrix saves the fitness value of each ants:

        f A11, A12 ,…, A1d

        f A21, A22 ,…, A2d

        M :

        (3)

        OA

        :

        Where,

        f An1, An2 ,…, And

        MOA = the matrix for storing the each ant fitness,

        Aij = the value of jth variable of ith ant, n = the total no. of ants and f =

        the objective function.

        So we suppose that ants as well as the antlions are hiding somewhere in the search area. So as to store their locations and fitness values, the following matrices are used:

        AL11 AL12 . . AL1d

        AL AL . . AL

        21 22 2d

        M Antlion

        . . . . .

        . . . . .

        (4)

        ALn1

        ALn2 . .

        ALnd

        Where: M Antlion = the matrix for storing the location of individual antlion, ants and d = the no. of variables.

        ALij = the value of jth variable of ith antlion, n = no. of

        f AL11, AL12 ,…, AL1d

        f AL21, AL22 ,…, AL2d

        M :

        (5)

        OAL

        :

        f ALn1, ALn2 ,…, ALnd

        Where, M OAL = the matrix for storing the fitness of individual antlion, and f = the objective function.

        ALij = the value of jth variable of ith antlion, n = no. of ants

      2. Random Walk of Ants

        Each of the behaviors is mathematically modeled as:

        The Random walks of ants is calculated as follows equation (6)

        (xt x ) * (d ct )

        xt i i i i c

        (6)

        i i

        i (d t a ) i

        Where, ai = the minimal of random walk of ith variable, bi = the Maximum of random walk in ith variable.

      3. Trapping in Antlions pits

        The Trapping in ant lions pits is calculated as follows equation (7) and equation (8)

        i j

        ct Antliont ct

        i j

        dt Antliont dt

      4. Sliding Ants towards Antlion

        The Sliding ants towards ant lion calculated as follows equation (9) and equation (10)

        t ct

        (7)

        (8)

        c (9)

        I

        t

        d t

        d (10)

        I

        Where, I = ratio, ct = the minimal of total variables at tth iteration, and dt = the vector containing the maximum of total variables at

        tth iteration.

      5. Catching prey and re-building the pit

        Catching prey and re-building the pits calculated as follows equation (11)

        Antliont

        Anttif [ f (Antt )] f (Antliont )

        (11)

        j i i j

        j i

        Where, t = the current iteration, Antlion t= the location of chosen jth antlion at tth iteration, and Ant t= the location of ith ant at tth

        iteration.

      6. Elitism

    Elitism of ant lion calculated using roulette wheel as follows equation (12)

    t Rt

    • Rt

      Anti

      A E

      A

      E

      2

      (12)

      Where,

      Rt = the random walk nearby the antlion chosen by means of the roulette wheel at tth iteration,

      Rt = the random walk

      nearby the elite at tth iteration,

      Antt = the location of ith ant at tth iteration.

      i

  3. ADAPTIVE ALO ALGORITHM

    In the meta-heuristic algorithms, randomization play a very important role in both exploration and exploitation where more randomization techniques are Markov chains, Levy flights and Gaussian or normal distribution and new technique is adaptive technique. Adaptive technique used by Pauline Ong in Cuckoo Search Algorithm (CSA) [2] and shows improvement in results of CSA algorithms. The Adaptive technique [3] includes best features like it consists of less parameter dependency, not required to define initial parameter and step size or position towards optimum solution is adaptively changes according to its functional fitness value o15ver the course of iteration. So mete-heuristic algorithms on integrated with adaptive technique results in less computational time to reach optimum solution, local minima avoidance and faster convergence.

    i t

    t 1 t

    1 ((bestf (t) fi(t)) (bestf (t) worstf (t)))

    Xi

    Where

    X randn *

    (13)

    X t 1 new solution of i-th dimension in t-th iteration

    i

    f (t) is the fitness value

  4. SIMULATION RESULTS FOR UNCONSTRAINT TEST BENCHMARK FUNCTION Table 1: Benchmark Test functions

    No. Name Function Dim Range Fmin

    f x x * R x

    F1 Sphere n

    2

    i

    10 [-100, 0

    100]

    F2 Schwefel 2.22

    i1

    n n

    f x x x

    * R x

    10 [-10, 0

    10]

    F3 Schwefel 1.2

    i1

    i i

    10

    [-100,

    100]

    0

    10

    [-100,

    0

    100]

    10

    [-30,

    0

    10

    [-100,

    0

    100]

    10

    [-1.28,

    0

    1.28]

    i1

    2

    n i

    f x x j * R x

    i1 j 1

    i

    F4 Schwefel 2.21

    f x max x

    F5

    Rosenbrocks

    Function f

    n1 2 2

    x 100x x

    i1 i

    F6

    Step Function

    n 2

    f

    x x 0.5 * R

    F7

    Quartic Function

    n

    i

    i1

    ,1 i n

    2

    xi 1

    * R x

    30]

    i x

    i1

    i

    f x ix4 random0,1* R x

    F8 Schwefel 2.26

    i1

    F x n x sin

    x *R x

    10 [-500,

    500]

    (- 418.9829*5

    F9 Rastrigin

    i i

    i1

    n

    i i

    F x x2 10cos 2 x 10 * R x

    )

    10 [-5.12, 0

    5.12]

    F10 Ackleys Function

    i1

    F x 20exp 0.2

    n

    1 2

    x

    i

    10 [-32, 0

    32]

    1 n

    n i1

    exp n cos 2 xi 20 e * R x

    F11 Griewank Function

    i1

    1 n n x

    10 [-600, 0

    F x

    x2 cos

    i

    1* R x

    600]

    i

    4000 i1

    i1

    i

    F12 Penalty 1

    n1

    10sin y y 12

    10 [-50, 0

    50]

    F x

    1 i

    i1

    n 110sin2 y

    y

    12

    y 1 xi 1 ,

    i 4

    k x

    i1

    • am

      n

      x a

      i

      u(x , a, k, m)

      i i

      0 a xi a

      k x

    • a m

    x a

    i i

    F13 Penalty 2

    10 [-50, 0

    n

    sin2 3 x x 12 50]

    1 i

    i1

    i

    F x 0.11 sin2 3 x 1

    x 12 1 sin2 2 x

    n

    n

    n

    F14 De Joung (Shekels Foxholes)

    u xi , 5,100, 4* R x

    i1

    1

    2 [-65.536, 1

    65.536]

    1 25 1

    F x

    500 j 1

    2

    6

    j xi aij

    i1

    F15 Kowaliks Function

    11 xi bi bi x2

    4 [-5,5] 0.00030

    2

    2

    f x ai b 2 b x

    • x

      F16 Shekel

      i1

      10

      i i

      3 4

      T

      1

      4 [0,10] -10.5363

      f x X ai X ai

      i1

    • ci

    F17 Cube function

    F18 Matyas function

    f x 100(x x3 )2 (1 x )2

    1 2 1 2

    2 1 1

    f (x) 0.26(x2 x2 ) 0.48x x

    30 [-100, 0

    100

    30 [-30, 0

    30]

    F19 Powell function

    D2 (x

    10x )2 5(x

    x )2 4 [-30, 0

    f (x) i1

    i i1

    i2

    30]

    i1 (x 2x

    )4 10(x

    x )4

    i i1

    i1

    i2

    F20 Beale Function

    1.5 x1 x x2

    2.25 x x x2

    230

    [-100, 0

    100]

    1 1 2

    2

    f (x) 1

    2.625 x x x3 2

    F21 levy13 function

    1 1 2

    2

    sin2 3 x x 1 1 sin2 3 x

    2

    30

    1 1

    [-10, 0

    10]

    f (x)

    x

    12 1 sin2 2 x

    2 2

    Table 2: Internal Parameters

    Parameter Name

    Search Agents no.

    Max. Iteration no.

    No. of Evolution

    F1-F21

    30

    500

    20-30

    Acoustic PD Localization

    40

    200

    20

    Note:- Scale specified on axis, Not specified means axis are linear scale

    F1 F2

    F3 F4

    F5 F6

    F7

    F8

    F9 F10

    F11 F12

    F13 F14

    F15 F16

    F17 F18

    F19 F20

    F21

    Fig. 1: Convergence Curve of Benchmark Test Function

    Table 3: Result for benchmark functions

    Fun.

    Ant-Lion optimizer (ALO)

    Adaptive Ant-Lion Optimizer (AALO)

    Ave

    Best

    S.D.

    Ave

    Best

    S.D.

    F1

    1.1018E-08

    8.5917E-09

    3.4308E-09

    6.9926E-09

    5.5958E-09

    3.4308E-09

    F2

    1.35

    0.0011442

    1.9076

    0.2666

    0.00052061

    1.9076

    F3

    0.05592

    0.0061171

    0.070433

    0.012982

    0.00077882

    0.070433

    F4

    0.0028435

    0.00058981

    0.0031871

    0.0011557

    0.00025095

    0.0031871

    F5

    8.8444

    8.2563

    0.83172

    1.5002

    7.6731E-06

    0.83172

    F6

    2.1803E-08

    1.0074E-08

    1.6588E-08

    1.0207E-08

    9.4448E-09

    1.6588E-08

    F7

    0.014989

    0.0062663

    0.012335

    0.027139

    0.0046907

    0.012335

    F8

    -2692.5959

    -3459.3448

    1084.3467

    -2850.0459

    -3656.8455

    1084.3467

    F9

    26.3663

    25.8689

    0.70354

    22.884

    19.8992

    0.70354

    F10

    0.5776

    5.544E-05

    0.81677

    5.4147E-05

    5.2544E-05

    0.81677

    F11

    0.1576

    0.14525

    0.017463

    0.2165

    0.1328

    0.017463

    F12

    1.5235

    0.98867

    0.75642

    0.31478

    0.31101

    0.75642

    F13

    3.9475E-07

    3.3722E-07

    8.1357E-08

    2.0961E-07

    4.28E-08

    8.1357E-08

    F14

    3.9604

    1.992

    2.7837

    2.4871

    1.992

    2.7837

    F15

    0.010793

    0.0011281

    0.013668

    0.00074227

    0.00073769

    6.4749E-06

    F23

    -3.8354

    -3.8354

    5.8935E-12

    -6.6715

    -10.5364

    5.4658

    F28

    3.5236

    2.4015E-11

    4.9831

    5.8609E-11

    2.3499E-11

    4.9652E-11

    F31

    6.0627E-14

    2.4656E-14

    5.0871E-14

    9.7097E-15

    2.403E-16

    1.3392E-14

    F34

    9.6533E-06

    5.7193E-06

    5.636E-06

    1.0075E-05

    3.4594E-06

    9.3556E-06

  5. ACOUSTIC PD LOCALIZATION SENSOR POSITION

Dielectric breakdown in transformers is most frequently initiated by partial discharges. The consequences of these types of occurrences can be hazardous if not detected in a timely fashion. Regular PD analysis gives an accurate indication of the status of the deterioration process. So it is possible to foretell developing fault condition by online monitoring and precautionary tests. It is very much essential to have information of PD level and location to plan maintenance of electrical equipment. A famous method of understanding the health of the transformer is by studying the partial discharge signals. Monitoring of transformer can be either online or offline. The primary established techniques for electrical PD detection by measuring current or Radio Frequency (RF) pulses. Suppression of interference is one of the main challenges in detecting PDs, either while the transformer is off-line or on- line in a noisy environment. The off-line PD detection methods only provide snapshots in time of part of the transformers condition. On the other hand, no standards have yet been developed for on-line electrical monitoring of PDs.

It is well known that the occurrence of discharge results in discharge current or voltage pulse, electromagnetic impulse radiation, ultrasonic impulse radiation and visible or ultraviolet light emission. Accordingly, there are several detection methods that have been developed to measure those phenomena respectively. Acoustic detection is one of them which is very famous nowadays.

PD generates acoustic waves in range of 20 kHz to 1 MHz. External system and internal system are two categories of acoustic detection techniques based on sensor location in transformer. External system is widely accepted as sensors are mounted outside of the transformer. An obvious advantage of the acoustic method is that it can locate the site of a PD by algorithms. Electromagnetic interference may cause corruption of signals captured by piezoelectric sensors.

A main objective is to determine the position of the PD source based on signals captured by sensor array inside the transformer tank as shown in Fig. 3. Each sensor will capture acoustic signals at different time as shown in Fig. 4. Time Difference of Arrival (TDOA) algorithm has been implemented to find location of partial discharge source.

PDE equation in homogeneous medium for propagation of acoustic wave:

2 P 22

2 2 P 2 P 2 P

t2

P x2 y2 z2

(14)

Where: P (x, y, z, t) pressure wave field; function of space and time; x, y, z Cartesian co-ordinates (mm) and v is acoustic wave velocity (m/s).

Sensor 4

x

Sensor 3

z

PD source

Sensor 1

Sensor 5

Sensor 2

y

Fig. 2: Visualization of PD source and sensor arrangement

U(t) PD

onset

T

S1 S2 S3 Sn

t21

t31

tn1

PD

Source

Time

Fig. 3: Schematic of acoustic time differences in reference to electrical PD signal Table 4: Transformer dimension and Co-ordination position of sensor

Element

X-axis (mm)

Y-axis (mm)

Z-axis (mm)

Transformer Dimension

5000

3000

4000

Actual PD source

4500

2600

3700

Sensor (S1)

2500

0

2000

Sensor (S2)

2500

1500

4000

Sensor (S3)

5000

1500

2000

Sensor (S4)

2500

3000

2000

Sensor (S5)

0

1500

2000

t1 =2600 micro-seconds ( Reference )

1() = [ 1600, 1500, 1900, 3524.69] 1 , = 2,3,4,5, And sensor 1 is assumed as reference paper [6]. Problem Formulation:

21 31

1000 1003 , 1100 1003 ,

(15)

41 51

700 1003 , 924.69 1003 ,

P x x 2 y y 2 z z 2 0.5

(16)

1 1 1

0.5

a x x 2 y y 2 z z 2 P ;

(17)

2 2 2

e 21

2 2 2 0.5

b x x3 y y3 z z3

P e31 ;

(18)

2 2 2 0.5

c x x4 y y4 z z4 /p>

P e41 ;

(19)

0.5

d x x 2 y y 2 z z 2 P ;

(20)

5 5 5

e 51

Min

{D (x, y, z, )} a2 b2 c2 d 2 ;

(21)

f e

Subjected to

0 x xmax

0 y ymax

0 z zmax

(22)

1200 e 1500, (m / s

Where:

, , and are transformer tank dimension and equality sound velocity.

Calculated PD source is Pc (xc , yc , zc ) comprehensive distance error of it with actual PD source

P(x, y, z) is

R x x

2 y y

2 z z

2 0.5

(23)

c c c

Error of each co-ordinate is formulated:

r

Lact Lcal Lact

100%

(24)

Maximum deviation Dmax

xact xcal

Dmax

max yact ycal

(25)

z

act zcal

Where; , ,, , , , actual and calculated co-ordinates respectively.

Table 5: Comparison of the results of PD localization

Coordinate (mm)

Actual PD source

ALO

AALO

GA

X

4500

4381.7459

4381.7465

4223.76

Y

2600

2469.6026

2469.603

2391.71

z

3700

3647.4901

3647.4905

3503.04

Table 6: Error analysis

Error

ALO

AALO

GA

Error of x%

2.627

2.627

6.14

Error of y%

5.015

5.322

8.01

Error of z%

1.419

1.419

5.32

D max /mm

130.3974

130.397

276.24

Comprehensive Error(del R/mm)

183.6975

183.6968

398.10

CONCLUSION

Ant Lion Optimizer have an ability to find out optimum solution with constrained handling which includes both equality and inequality constraints. While obtaining optimum solution constraint limits should not be violated. Randomization plays an important role in both exploration and exploitation. Adaptive technique causes faster convergence, randomness, and stochastic behavior for improving solutions. Adaptive technique also used for random walk in search space when no neighboring solution exits to converse towards optimal solution. Acoustic PD source localization method based on AALO algorithm is feasible. PD localization by AALO gives better result than ALO algorithm and also accurate in compare to GA. The ALO result of various unconstrained problems proves that it is also an effective method in solving challenging problems with unknown search space.

ACKNOWLEDGMENT

The authors would also like to thank Prof. Seyedali Mirjalili for his valuable comments and support. http://www.alimirjalili.com/ALO.html.

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