Journal of Computational Science and Technology | |
PSO/GA Hybrid Method and Its Application to Supersonic-Transport Wing Design | |
Yoshikazu MAKINO1  Kazuhisa CHIBA1  Takeshi TAKATOYA1  | |
[1] Japan Aerospace Exploration Agency | |
关键词: Evolutionary Algorithms; Multi-Objectives; Multidisciplinary Design Optimization; Aerodynamics; Composite Structures; Boom Noise; | |
DOI : 10.1299/jcst.2.268 | |
学科分类:地球科学(综合) | |
来源: Japan Academy | |
【 摘 要 】
References(25)Cited-By(1)The hybrid method between multi-objective particle swarm optimization and adaptive range multi-objective genetic algorithm has been developed and its performance has been measured by using three test functions with noise. Moreover, it was applied to a large-scale and real-world engineering design problem. The performance measurement was carried out under the conditions of a small number of population size and generations to apply the practical problem which it needed large computational time for the evaluation. The convergence metric and the cover rate were employed as the measurement manners. Consequently, it revealed that the present hybrid method had similar performance for a simple three-dimensional test problem compared with genetic algorithm in a small number of generations. Moreover, it had the best performance for the test functions with noise. Therefore, the present hybrid method was applied to the wing design of the silent supersonic technology demonstrator. As a result, the efficient design exploration was performed and obtained 75 non-dominated solutions revealed the beneficial knowledge to decide a compromise solution.
【 授权许可】
Unknown
【 预 览 】
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RO201912010158409ZK.pdf | 2268KB | download |