An efficient metamodel-based multi-objective multidisciplinary design optimization framework

被引:23
作者
Zadeh, Parviz Mohammad [1 ]
Sayadi, Mohsen [1 ]
Kosari, Amirreza [1 ]
机构
[1] Univ Tehran, Fac New Sci & Technol, Tehran, Iran
关键词
Multi-objective optimization; Particle swarm optimization (PSO); Metamodel; Multidisciplinary design optimization (MDO); Unmanned aerial vehicles (UAV); COLLABORATIVE OPTIMIZATION; PARTICLE SWARM; EVOLUTIONARY ALGORITHM; APPROXIMATION; CONSTRUCTION; CONVERGENCE; MODEL;
D O I
10.1016/j.asoc.2018.09.014
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
This paper presents an efficient metamodel-based multi-objective multidisciplinary design optimization (MDO) architecture for solving multi-objective high fidelity MDO problems. One of the important features of the proposed method is the development of an efficient surrogate model-based multi-objective particle swarm optimization (EMOPSO) algorithm, which is integrated with a computationally efficient metamodel-based MDO architecture. The proposed EMOPSO algorithm is based on sorted Pareto front crowding distance, utilizing star topology. In addition, a constraint-handling mechanism in non-domination appointment and fuzzy logic is also introduced to overcome feasibility complexity and rapid identification of optimum design point on the Pareto front. The proposed algorithm is implemented on a metamodel-based collaborative optimization architecture. The proposed method is evaluated and compared with existing multi-objective optimization algorithms such as multi-objective particle swarm optimization (MOPSO) and non-dominated sorting genetic algorithm II (NSGA-II), using a number of well-known benchmark problems. One of the important results observed is that the proposed EMOPSO algorithm provides high diversity with fast convergence speed as compared to other algorithms. The proposed method is also applied to a multi-objective collaborative optimization of unmanned aerial vehicle wing based on high fidelity models involving structures and aerodynamics disciplines. The results obtained show that the proposed method provides an effective way of solving multi-objective multidisciplinary design optimization problem using high fidelity models. (C) 2018 Elsevier B.V. All rights reserved.
引用
收藏
页码:760 / 782
页数:23
相关论文
共 84 条
[1]  
[Anonymous], 2004, P 45 AIAA ASME ASCE
[2]  
[Anonymous], 2015, THESIS
[3]  
[Anonymous], 2016, FUZZY LOGIC ENG APPL
[4]  
[Anonymous], 4 WORLD C STRUCT MUL
[5]  
[Anonymous], 2010, WATER RESOUR RES
[6]  
[Anonymous], 2006, P 44 AIAA AER SCI M
[7]   A survey of multidisciplinary design optimization methods in launch vehicle design [J].
Balesdent, Mathieu ;
Berend, Nicolas ;
Depince, Philippe ;
Chriette, Abdelhamid .
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2012, 45 (05) :619-642
[8]   Execution of multidisciplinary design optimization approaches on common test problems [J].
Balling, RJ ;
Wilkinson, CA .
AIAA JOURNAL, 1997, 35 (01) :178-186
[9]  
Bansal J.C., 2011, Em 2011 Third World Congress on Nature and Biologically Inspired Computing, paginas, P633, DOI DOI 10.1109/NABIC.2011.6089659
[10]  
Binh T.T., 1997, 3 INT C GEN ALG MEND, V25, P27