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Hybrid Gravitational Search Flower Pollination Algorithm for Combined Economic Emission Load Dispatch
1.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1485 HYBRID GRAVITATIONAL SEARCH FLOWER POLLINATION ALGORITHM FOR COMBINED ECONOMIC EMISSION LOAD DISPATCH Man Mehak Sidhu1, Shivani Mehta2 1Lecturer, Dept. Of Electrical, B.F.C.E.T, Bathinda, Punjab, India 2Assitant Professor, Dept. Of Electrical, D.A.V.E.T, Jalandhar, Punjab, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Economic Load Dispatch is the most remarkableprobleminoptimizationforforecastingthegenerationintheareaof thermal generating units in power system .Combined economic and emission load dispatch determines the optimal generation of the power system by minimizing the fuel cost and emission levels simultaneously. In this work, a new Hybrid Gravitational Search Flower Pollination (GSFPA) based algorithm is proposed for achieving improved results in the ELD problem where gravitational search is used to decide the step size in levy flight mechanism. In the new technique gravitational search algorithm works in coordination with flower pollination algorithm to find desired and refined results. The proposed algorithm will be tested for IEEE 14 and 39 bus system to prove its credibility. This algorithm has less number of operators and hence it can be easily coded in any programming language. To prove the feasibility of this algorithm its performance is compared with other existing algorithms. Key Words: CEED, PBO, GSFPA, ELD, PSO 1.INTRODUCTION In today’s modern era of electrical power plays a very vital role to survive and to meet variousdemands.Inorderto meetthese demands the generation, transmission and distribution of power must be optimized efficiently. Economic operation of power systems is met by meeting the load demand through optimal scheduling of power generation. Minimization of fuel cost is the main objective of finest power flow (OPF) problems. Optimal real power scheduling will guarantee economic benefits to the power system operators and reduce the release of polluting gases.ELD primarily aims at optimal scheduling of real power generation from committed units in such manner that it meets the total demand and losses while satisfying the constraints [10]. Achieving minimum cost while satisfying the constraints makes the ELD problem a highly non-linear constrained optimization problem. The non linearity of the difficulty is due to non linearity and valve point effects of input–output characteristics of generating units. The aim of cost minimization may have multiple local optima.Thereisalwaysa demandfor a proficient optimization technique for these kinds of highly non linear objective functions. Further, the algorithm is expected to produce accurate results for the ELD problem. In the last decade, several bio inspired algorithms are introduced and attempted formanyengineeringoptimizationproblems. Some of the notable bio inspired algorithms are particle swarm optimization algorithm (PSO), a well received algorithm and utilized in almost all engineering applications successfully. Firefly algorithm is another recently introduced algorithm for engineering optimization that has been effectively used to solve the dynamic ELD problem. Theses algorithms are highly successful and cannot be easily trapped in to local optima. In addition, they are comfortable with all types of objective functions. Flower pollination algorithm FPA is one such nature inspired algorithm developed by Xin She Yang [7]-[8] for engineering tasks. The efficiency of nature/bio inspired algorithms is proved to be outperforming eventheevolutionary basedalgorithms.Inthis paper, the new Hybrid Gravitational Search Flower Pollination based algorithm has been proposed for achieving improved results in the ELD problem where gravitational search is used to decide the step size in levy flight mechanism. This algorithm has lesser number of operators and hence can be easily coded in any programming language. To prove the strength of this algorithm its performance is compared with other existing algorithms. 1.1 Working of Hybrid Gravitational Search Flower Pollination Algorithm:- Based on the concept of gravitational search and flower pollination, gravitational search pollination algorithm (GSFPA) is developed. Rule1. Biotic and cross-pollination are considered as global pollination process and pollen is carried by a movement which obeys Levy flight movement incorporating gravitational search capability. Rule2. A biotic and self-pollination are equivalent to local pollinationprocessincorporatingupdatingofgravitational equation. Rule3. Pollinators can develop flower constancy, which is like reproduction probability and proportional to the similarity of two flowers involved.
2.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1486 Rule4. Changing from local pollination to global pollination or vice versa can be controlled by a probability p ϵ[0, 1]. For implementation of this FPA algorithm, a set of updating formulae are developed by converting the rules into updating equations. In the global pollination step, flower pollen gametes are carried by pollinatorssuchasinsectsoverlongerdistances. Therefore, the mathematical equivalent of Rule 1 and flower constancy is written as Where, is the solution vector (pollen) xi at iteration t, xis the current best solution, t/TeGo is a gravitational scaling factor to control the step size. L(λ) is the parameter that corresponds to the strengthofthepollination,whichessentiallyis also the step size. Since insects may move over a long distance with various distance steps, we can use a Levyflight to mimic this characteristic efficiently. That is, we draw L > 0 from a Levy distribution Here, G(t) is the standard gamma distribution valid for large steps. i.e. for s > 0. Then, to model the local pollination, both Rule 2 and Rule 3 can be represented as: Where and are pollen from different flowers of the same plant species. This essentially mimics the flower constancy ina limited neighborhood. Mathematically, if and comes from the same species or selected from the same population, this equivalently becomes a local random walk if we draw from a uniform distribution in [0, 1].Pollination may also occur in a flower from the neighboring flower than by the far away flowers. In order to copy this, a switch probability (Rule 4) is used through a proximity probability p to switch between global pollination andlocal pollination.Apreliminaryparametricshowed that p=0.8 might work better for most applications.
3.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1487 NO YES Fig 1. Flow chart for GSFPA START Read data of electrical thermal units and load demand(Cost coefficients a, b, c and power demand, constraints) Intialize the input parameters n, p, iterations T ,c of flower pollination and gravity search algorithm Set the iteration counter Initialize the random position of population of objective cost function (power generation values) Check if value of p<0.8 Perform levy flight distribution with to select optimal step size and global pollination Perform G(t) distribution and local pollination Evaluate new solution of power generation, cost .if new solution is less than previous solution, update in the population. Check iteration counter and constraints like power generation limits, Find the current best solution Display Result of power generation, fuel cost STOP (t))X-(t)(X*c+(t))/RM*(t)(M*G(t)=F idjdijjiijd
4.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1488 2. RESULTS 2.1 INPUT DATA Table 1.Input data for 14 bus, 6 generator system [18] Unit ($/h) ($/MWh) ($/( )h) 1 10 125 756.9888 38.5390 0.15247 2 10 150 451.3251 46.1591 0.10587 3 35 210 1243.5311 38.3055 0.03546 4 35 225 1049.9977 40.3965 0.02803 5 125 315 1356.6592 38.2704 0.01799 6 130 325 1658.5696 36.3278 0.02111 Fig 2. B-Coefficients for 14 Bus, 6 Generator System [18] Table 2. Input Data for 39 Bus System [18] Unit ($/h) ($/MWh) ($/( )h) 1 10 55 1000.403 40.5407 0.12951 2 20 80 950.606 39.5804 0.10908 3 47 120 900.705 36.5104 0.12511 4 20 130 800.705 39.5104 0.12111 5 50 160 756.799 38.5390 0.15247 6 70 240 451.325 46.1592 0.10587 7 60 300 1243.531 38.3055 0.03546 8 70 340 1049.998 40.3965 0.02803 9 135 470 1658.569 36.3278 0.02111 10 150 470 1356.659 38.2704 0.01799
5.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1489 Fig 3. B-Coefficients for 39 Bus System [18] 2.2 RESULTS OBTAINED FOR MULTIOBJECTIVE ECONOMIC LOAD DISPATCH Table 3. Cost comparison and power generation for 6 unit system The table above shows the comparison of power dispatch and fuel cost of 6 generators, 14 bus system usingflowerpollination optimization technique. The above results clearly state that the power loss, fuel cost and computational time taken by flower pollination optimization is less as compared to other various techniques Table 4. Losses of various techniques for CEED problem Sr.n o. Method Power demand (MW) P1 (MW) P2 (MW) P3 (MW) P4 (MW) P5 (MW) CPU Time(se conds) P6 (MW) Emissi on (kg) Fuel Cost ($) 1 GSFPA [propose d work 2] 1200 85.73 93.24 209.72 227.45 324.76 3.16 356.16 1282 64312. 7 2 FPA [propose d work 1] 1200 91.24 96.26 215.38 245.43 323.19 3.12 342.72 1284 64762. 8 2 MODE [18] 1200 108.628 4 115.94 56 206.796 9 210.000 0 301.888 4 3.09 308.412 7 1286 64843 3 PDE [18] 1200 107.396 5 122.14 18 206.753 6 203.704 7 308.104 5 3.52 303.379 7 1281 64920 4 NSGA II[18] 1200 113.125 9 116.44 88 217.419 1 207.949 2 304.664 1 5.05 291.596 9 1285 64962 5 SPEA 2[18] 1200 104.157 3 122.98 07 214.955 3 203.138 7 316.030 2 7.42 289.939 6 1285 64884 Technique Losses(MW) GSFPO 51.42 FPA 51.47 MODE 51.61 PDE 51.78 NSGA II 52.12 SPEA2 51.15
6.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1490 Table 5. Weight Values and output IEEE 6 unit system Fig 4. Cost and Emission Comparison Graph for Various Optimization Techniques The graph shown above represents the fuel cost and emissions for various optimization techniques implemented on a 14 bus, 6generator system. The comparison shows that the cost using pollination based algorithm technique is the minimum of all other techniques. Table 6. IEEE 10 unit system Result for CEED Problem W1 W2 Fuel Cost Emission(kg) 0.25 0.75 64362.9 1287 0.5 0.5 64572.8 1284 0.75 0.25 64577.4 1285 0.35 0.65 64312.7 1282 0.60 0.40 64122.4 1309 0.40 0.60 65314.2 1278 S.No Method GSFPO [proposed work 2] FPA[proposed work 1] MODE [18] PDE [18] NSGA II [18] SPEA 2 [18] Power demand (MW 2000 2000 2000 2000 2000 2000 1 P1 (MW) 47.28 51.44 54.9487 54.9853 51.9515 52.9761 2 P2(MW) 86.45 82.45 74.5821 79.3803 67.2584 72.8130 3 P3(MW) 89.54 89.67 74.4294 83.9842 73.6879 78.1128 4 P4(MW) 126.21 134.25 80.6875 86.5942 91.3554 83.6088
7.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1491 The table above shows the comparison of power dispatch and fuel cost of 10 generator, 39 bussystemusingflower pollination optimization technique. The above results clearly state that the power loss, fuel cost and computational time taken by flower pollination optimization is less as compared to other various techniques TABLE 7.Weight Values and output for IEEE 10unit system Table 8.Losses of various techniques for CEED problem 5 P5(MW) 81.44 82.59 136.8551 144.4386 134.0522 137.2432 6 P6(MW) 98.58 92.13 172.6393 165.7756 174.9504 172.9188 7 P7(MW) 278.29 278.46 283.8233 283.2122 289.4350 287.2023 8 P8(MW) 335.89 321.78 316.3407 312.7709 314.0556 326.4023 9 P9(MW) 466.91 455.89 448.5923 440.1135 455.6978 448.8814 10 P10(MW) 468.34 439.96 436.4287 432.6783 431.8054 423.9025 Emission(Kg) 4114.67 4123.78 4124.90 4111.40 4130.20 4109.10 CPU Time(sec) 4.12 3.78 3.82 4.23 6.02 7.53 FUEL COST 108965 110177 113480 113510 113540 113520 W1 W2 Fuel Cost Emission(kg) 0.25 0.75 113586 4122.92 0.5 0.5 111897 4125.89 0.75 0.25 108965 4114.67 0.35 0.65 124598 4112.93 0.60 0.40 118432 4118.37 0.40 0.60 116423 4113.76 Technique Losses(MW) GSFPO 84.58 PBO 84.89 MODE 84.64 PDE 84.69 NSGA II 84.81 SPEA 2 84.52
8.
International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1492 Fig 5. Cost and Emissions Comparison Graph for Various Optimization Techniques The graph shown above represents the fuel cost and emissions for various optimization techniques implemented on a 39 bus, 10 generator system. The comparison shows that the cost using pollination based algorithm technique is the minimum of all other techniques. The results show that the value of power output, fuel cost obtained and losses incurred by gravitational search flower pollination based optimization technique is better than other optimization techniques 4. CONCLUSIONS In this paper hybrid gravitational search flower pollination algorithm (FPA) has been implementedtomultiobjectiveproblem considering both cost and emission constraints for economic load dispatch. The said algorithm works on the basis of pollinating behavior of flowering plants. Contrasting to the other bio inspired optimization techniques, FPA utilizes levy flight mechanism to generate population for the next generations. In the hybrid algorithm gravitational search algorithm (GSFP0) is imposed along with pollination optimization to enhance the results. The said algorithm can be easily modified according to different problems and the algorithm is highly efficient as it does not have the complication of very large number of parameters. The algorithm can be easily coded in any programming language. The proposed hybrid algorithm has been used and tested for IEEE 14 and 39 bus systems and the results achieved have shown to improve the optimization of the combined economic and emission dispatch problem. The results obtained by the above mentioned GSFPO algorithm when tested on Case I and II were far better than those obtained by the existing algorithmsinthe given literature. The given hybrid algorithm has lesser number of operators which minimizes the chances of solutions to get trapped in the local minima. The computational time ofthefollowingalgorithmisalsolessthantheexistingalgorithms.Further the said algorithm can be tested for bigger systems. The results obtained are found to be superior and heartening 5. REFERNCES [1] A.Y. Abdelaziz, E.S. Ali, S.M. Abd Elazim, Flower pollination algorithm to solve combined economic and emission dispatch problems , Engineering Science and Technology, 19 (2016) [2] D.Vigneshwaran, R.Sivakumar, S.Vijayaraj, Flower Pollination Algorithm for Economic Dispatch Problem with Prohibited Zones, Ramp Rate Limits & Multi-Fuel Options International Journal of Advanced Research in Electrical, Electronics and Instrumentation Engineering (An ISO 3297: 2007 Certified Organization) Vol. 4, Issue 11, November (2015) [3] Kamalam Balasubramani1, Karnan Marcus , A Study on Flower Pollination Algorithm and Its Applications International Journal of Application or Innovation in Engineering & Management Volume 3, Issue 11, ISSN 2319 – 4847, November 2014 )
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International Research Journal
of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 07 | July -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 1493 [4] Prathiba, Flower pollination algorithm applied for different economic load dispatch problems. International Journal of Engineering and Technology, ISSN: 0975-4024, Vol 6, No 2, May(2014) [5] S. Chetan Varma, K.S. Linga Murthy, K.SriChandan,GaussianParticleSwarmOptimizationforCombinedEconomicEmission Dispatch, 978-1-4673-6150-7/13/ ©(2013) IEEE [6] Mugdha Udgir, Hari Mohan Dubey, Manjaree Pandit , Gravitational Search Algorithm: A Novel Optimization Approach for Economic Load Dispatch” International Conference on Microelectronics, Communication and Renewable Energy (2013) [7] Xin-She Yang, Mehmet Karamanoglu, Xingshi He, Multi-objective Flower Algorithm for Optimization International Conference on Computational Science, ICCS (2013) [8]Xin-She Yang, Flower Pollination Algorithm for Global Optimization, Dec (2013) [9] Deepan B,Janani R , A Real Coded Genetic Algorithm For Solving Combined Economic Emission Dispatch (CEED) With Practical Constraints International Journal of Engineering Research&Technology,ISSN:2278-0181www.ijert.org Vol.2Issue 6, June (2013) [10] D. P. Kothari, Yadwinder Singh Brar, Harinder Pal Singh, Multiobjective Load DispatchUsingParticleSwarmOptimization ,IEEE 8th Conference on Industrial Electronics and Applications(2013). [11] Sai H. Ling, Herbert H. C. Iu, Kit Y. Chan and Shu K. Ki , Economic Load Dispatch: A New Hybrid Particle Swarm Optimization Approach. Australasian universities power engineering conference (2007) [12] N. A. Rahmat, and I. Musirin, Differential EvolutionAntColonyOptimization(DEACO)TechniqueinSolvingEconomicLoad Dispatch Problem. IEEE power engineering and optimization conference, June (2012) [13] Sunny Orike , David W. Corne , Improved Evolutionary Algorithms for Economic Load Dispatch Optimization Problems”. 12th UK workshop on computational intelligence, (2012) [14] Gaurav Prasad Dixit, Hari Mohan Dubey, Manjaree Pandit,B.K.Panigrahi,Artificial BeeColonyOptimizationforCombined Economic Load and Emission Dispatch Second International Conference on Sustainable Energy and Intelligent System(2011) [15] G. Suganya K. Balamurugan Dr. V. Dharmalingam Multi-Objective Evolutionary Programming Technique for Economic/Emission Load Dispatch IEEE- International Conference on Advances in Engineering, Science and Management March 30, 31, (2012). [16] I. A. Farhan , and M. E. El-Hawary , Multi-Objective Economic-Emission Optimal Load Dispatch Using Bacterial Foraging Algorithm , 2012 25th IEEE Canadian Conference on Electrical and Computer Engineering (2012) [17] Luis Bayón, José M. Grau , María M. Ruiz , and Pedro M. Suárez , The Exact Solution of the Environmental/Economic Dispatch Problem. IEEE Transactions On Power Systems, Vol. 27, No. 2, May (2012) [18] M.Basu “Economic environmental dispatch using multiobjective differential evolution Applied SoftComputing Vol II pp.2845-2853 ,(2011) [19] Kirschen, Daniel (2010). Fundamentals of Power System Economics. Wiley. ISBN 0-470-84572-4. [20] Mahor, Economic dispatch using particle swarm optimization: A review. IEEETransactionsonPowerSystems, Vol.27,No. 2, June (2009) [21] Park,A Particle Swarm Optimization for Economic Dispatch with Non Smooth Cost Functions.IEEE transactions on power systems, vol. 20, no. 1, February (2005). [22] Zwee-le-Gang, Particle swarm optimization to solving the economic dispatch considering the generator constraints. IEEE Transactions on Power Systems , Volume: 18, Issue: 3, Aug.( 2003 ) [23] Ray D. Zimmerman, Hsiao-Dong Chiang, “Fast Decoupled Power Flow for Unbalanced Radial Distribution Systems” IEEE Transactions on Power Systems (1995) [24] Sidhartha Panda, R.N.Patel, N.P.Padhy , Power System Stability Improvement by TCSC Controller Employing a Multi- Objective Genetic Algorithm Approach. International Journal ofElectrical,Computer,Energetic,ElectronicandCommunication Engineering Vol:1, No:2, (2007) [25] Esmat Rashedi, Hossein Nezamabadi-pour, Saeid Saryazdi, GSA: A Gravitational Search Algorithm, Information Sciences Journal, Volume 179 Issue, June(2009 )
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