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基于模糊评判与优化的微型扑翼飞行器扑动机构综合设计方法
引用本文:邵立民,宋笔锋,李为吉.基于模糊评判与优化的微型扑翼飞行器扑动机构综合设计方法[J].机械设计,2007,24(9):28-32.
作者姓名:邵立民  宋笔锋  李为吉
作者单位:西北工业大学,航空学院,陕西西安,710072
基金项目:总装气动预研资助项目 , 国防科技应用基础研究基金
摘    要:针对微型扑翼飞行器曲柄摇臂扑动机构,提出了影响扑动机构综合性能档方法对多种曲柄摇臂扑动机构方案进行优选,并对获选方案进行优化设计,在此基础上形成了微型扑翼飞行器扑动机构综合设计方法.样机研制和外场试飞证明了文中方法对提高扑动机构综合性能是有效的.

关 键 词:微型扑翼飞行器  扑动机构  模糊评判  优化设计  模糊评判  优化设计  微型扑翼飞行器  机构综合  设计方法  optimization  fuzzy  judgement  based  aircraft  mechanism  flapping  method  designing  试飞  样机研制  机构方案  优选  性能  影响  曲柄
文章编号:1001-2354(2007)09-0028-04
修稿时间:2006-07-31

Synthesized designing method on flapping mechanism of minityped flapping-wing aircraft based on fuzzy judgement and optimization
SHAO Li-min,SONG Bi-feng,LI Wei-ji.Synthesized designing method on flapping mechanism of minityped flapping-wing aircraft based on fuzzy judgement and optimization[J].Journal of Machine Design,2007,24(9):28-32.
Authors:SHAO Li-min  SONG Bi-feng  LI Wei-ji
Abstract:Directed against the crank-rocker flapping mechanism of minityped flapping-wing aircraft,six items of key influencing factors that affects the synthetic properties of flapping mechanism were put forward.Using the fuzzy judging method to carrying out optimization on manifold schemes of crank-rocker flapping mechanism,and carrying through optimization design on the being selected scheme and on this basis formed synthetic designing method of flapping mechanism of minityped flapping aircraft.Prototype development and outer field test flight testified that the method of this paper is effective for enhancing the synthetic property of flapping mechanism.
Keywords:minityped flapping aircraft  flapping mechanism  fuzzy judgement  optimization design
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