首页 | 本学科首页   官方微博 | 高级检索  
     

平流层飞艇的多目标优化与决策
引用本文:孙晓颖, 李天娥, 陆正争, 武岳, 王长国. 平流层飞艇的多目标优化与决策[J]. 工程力学, 2015, 32(6): 243-250. DOI: 10.6052/j.issn.1000-4750.2013.11.1106
作者姓名:孙晓颖  李天娥  陆正争  武岳  王长国
作者单位:1.结构工程灾变与控制教育部重点实验室(哈尔滨工业大学),黑龙江,哈尔滨 150090;;2.哈尔滨工业大学土木工程学院,哈尔滨 150090;;3.中国航天建设集团. 北京 100071;;4.哈尔滨工业大学复合材料与结构研究所,哈尔滨 150080
基金项目:国家自然科学基金项目(50908068,91215302); 航空科学基金项目(2013ZA77001)
摘    要:该文建立了以平流层飞艇阻力最小、自重最轻、极限承载力最大及刚度最大为优化目标的多目标优化模型;采用强度Pareto进化算法(SPEA)进行了多目标优化设计;基于优化所得的Pareto解集,采用基于信噪比的决策方法选择满足实际需要的最终方案。结果表明:采用的SPEA算法是合理有效的,可以得到非劣解分布较均匀的Pareto曲面;通过基于信噪比的决策方法,可从非劣解集中获得满足实际要求的最稳健设计方案。

关 键 词:平流层飞艇  多目标优化  SPEA  Pareto前沿  多目标决策  信噪比
收稿时间:2013-11-26
修稿时间:2014-04-01

MULTI-OBJECTIVE OPTIMIZATION AND DECISION MAKING OF STRATOSPHERE AIRSHIPS
SUN Xiao-ying, LI Tian-e, LU Zheng-zheng, WU Yue, WANG Chang-guo. MULTI-OBJECTIVE OPTIMIZATION AND DECISION MAKING OF STRATOSPHERE AIRSHIPS[J]. Engineering Mechanics, 2015, 32(6): 243-250. DOI: 10.6052/j.issn.1000-4750.2013.11.1106
Authors:SUN Xiao-ying  LI Tian-e  LU Zheng-zheng  WU Yue  WANG Chang-guo
Affiliation:1.Key Laboratory of Structural Engineering and Control, Ministry of Education, China (Harbin Institute of Technology), Heilongjiang, Harbin 150090, China;;2.School of Civil Engineering, Harbin Institute of Technology, Harbin 150090, China;;3.China Aerospace Construction Group Co., Ltd, Beijing 100071, China;;4.Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China
Abstract:A multi-objective optimization model for the design of stratosphere airships is proposed, which aims at minimizing the drag force and the weight, whilst maximizing the ultimate strength and stiffness of airships. SPEA (Strength Pareto Evolutionary Algorithm) method is used for the multi-objective optimization design. SNR (Signal-to-Noise Ratio)-based decision method is applied to determine the final design from the Pareto solution set derived from the optimization computation. This study demonstrates that the application of the SPEA method is effective and efficient in obtaining the Pareto surface with uniform non-inferior solutions. Based on the SNR-based decision method, the optimal design solution, which satisfies the actual needs, can be efficiently identified from the non-inferior solution set.
Keywords:stratosphere airship  multi-objective optimization  SPEA  Pareto front  multi-objective decision  SNR
本文献已被 CNKI 等数据库收录!
点击此处可从《工程力学》浏览原始摘要信息
点击此处可从《工程力学》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号