Butterfly optimization algorithm: a novel approach for global optimization
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"Butterfly optimization algorithm: a..." refers background in this paper
...InGA, a problem solution is considered as the individual’s chromosome and a population of such individuals strives to survive under harsh conditions (Holland 1992; Goldberg and Holland 1988)....
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...Up to now, researchers have only used very limited characteristics inspired by nature and there is room for more algorithm development (Yang 2010a; Onwubolu and Babu 2004; Wolpert and Macready 1997)....
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"Butterfly optimization algorithm: a..." refers methods in this paper
...…)2]} σ( −→x ) = 6PL x4x 2 3 δ( −→x ) = 4PL 3 Ex23 x + x4 Pc( −→x ) = 4.013E √ x23 x 6 4 36 L2 ( 1 − x3 2L √ E 4G ) P = 6000 lb,L = 14 in., δmax = 0.25 in., E = 30 × 106 psi, G = 12 × 106 psi, τmax = 13600 psi, σmax = 30000 psi (6) In the past, this problem is solved by GWO (Mirjalili et al. 2014),…...
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...The heuristic methods that have been adopted to optimize this problem are: Chaotic variant of Accelerated PSO (CAPSO) (Gandomi et al. 2013b), Table 7 Comparison results of welded beam design problem Algorithm Optimum variables Optimum cost h l t b BOA 0.1736 2.9690 8.7637 0.2188 1.6644 GWO 0.2056 3.4783 9.0368 0.2057 1.7262 GSA 0.1821 3.8569 10.0000 0.2023 1.8799 GA1 N/A N/A N/A N/A 1.8245 GA2 N/A N/A N/A N/A 2.3800 GA3 0.2489 6.1730 8.1789 0.2533 2.4331 HS 0.2442 6.2231 8.2915 0.2443 2.3807 Random 0.4575 4.7313 5.0853 0.6600 4.1185 Simplex 0.2792 5.6256 7.7512 0.2796 2.5307 David 0.2434 6.2552 8.2915 0.2444 2.3841 Approx 0.2444 6.2189 8.2915 0.2444 2.3815 Fig....
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...The mathematical formulation is as follows: Consider −→x = [x1x2x3x4] = [hltb], Minimize f (−→x ) = 1.10471x21 x2 + 0.04811x3x4(14.0 + x2), Subject to g1( −→x ) = τ(−→x ) − τmax ≤ 0, g2( −→x ) = σ(−→x ) − σmax ≤ 0, g3( −→x ) = δ(−→x ) − δmax ≤ 0, g4( −→x ) = x1 − x4 ≤ 0, g5( −→x ) = P − Pc(−→x ) ≤ 0, g6( −→x ) = 0.125 − x1 ≤ 0, g7( −→x ) = 1.10471x21 + 0.04811x3x4(14.0 + x2) − 5.0 ≤ 0, Variable range 0.1 ≤ x1 ≤ 2, 0.1 ≤ x2 ≤ 10, 0.1 ≤ x3 ≤ 10, 0.1 ≤ x4 ≤ 2 (5) where τ(−→x ) = √ (τ ′)2 + 2τ ′(τ ′′) x2 2R + τ ′′2 τ ′ = P√ 2x1x2 τ ′′ = MR J Table 6 Comparison of results for spring design problem Algorithm Optimum variables Optimum weight d D N BOA 0.051343 0.334871 12.922700 0.0119656 GWO 0.051690 0.356760 11.288110 0.0126615 GSA 0.050276 0.323680 13.525410 0.0127022 PSO 0.051728 0.357644 11.244543 0.0126747 ES 0.051989 0.363965 10.890522 0.0126810 GA 0.051480 0.351661 11.632201 0.0127048 HS 0.051154 0.349871 12.076432 0.0126706 DE 0.051609 0.354714 11.410831 0.0126702 Mathematical optimization 0.053396 0.399180 9.1854000 0.0127303 Constraint correction 0.050000 0.315900 14.250000 0.0128334 M = P ( L + x2 2 ) R = √ x22 4 + ( x1 + x3 2 )2 J = 2 {√ 2x1x2 [ x22 4 ( x1 + x3 2 )2]} σ( −→x ) = 6PL x4x 2 3 δ( −→x ) = 4PL 3 Ex23 x + x4 Pc( −→x ) = 4.013E √ x23 x 6 4 36 L2 ( 1 − x3 2L √ E 4G ) P = 6000 lb,L = 14 in., δmax = 0.25 in., E = 30 × 106 psi, G = 12 × 106 psi, τmax = 13600 psi, σmax = 30000 psi (6) In the past, this problem is solved by GWO (Mirjalili et al. 2014), GSA (Rashedi et al. 2009), GA1 (Coello 2000b), GA2 (Deb 1991), GA3 (Deb 2000) and HS (Lee and Geem 2005)....
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...The simulation results ofBOAare com- pared with Grey Wolf Optimization (GWO) (Mirjalili et al. 2014), Gravitational Search Algorithm (GSA) (Rashedi et al. 2009), PSO (He and Wang 2007), ES (Mezura-Montes and Coello 2008), GA (Coello 2000a), HS (Mahdavi et al. 2007), and DE (Huang et al. 2007)....
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