期刊文献+

BP神经网络预测降落伞绸透气性的研究 被引量:5

A study of prediction of air permeability of the parachute fabric by BP neural network
下载PDF
导出
摘要 透气性是降落伞绸的重要性能指标。降落伞绸织物的纱线线密度和织物密度、厚度、面密度及织物组织等结构参数与其透气量存在非线性的关系,由于织物结构各参数间的非线性关系及多个影响因素共同对织物的透气性能的作用,织物结构参数与其透气性能之间很难用传统数学、力学的方法来描述。人工神经网络能够处理复杂的非线性关系。本课题研究了利用人工神经网络来预测降落伞绸织物的透气性能,以期代替传统的测试方法,从而在新品种设计时对织物的参数设定提供指导。 The air permeability is an important parameter describing the fabric function of parachute. It is influenced by multiple factors of the fabric attribute such as fabric density and thickness, threads per unit length, the fabric area density, and weave structure, etc. The relationship between the air permeability and these factors is nonlinear. The nonlinear relationship is difficulty to build by traditional mathematical and mechanical methods. By taking advantage of BP neural network method that can handle the complicated non-linearity, this paper studies the prediction of air permeability based on fabric attribute, trying to introduce a new method that advances the traditional ones for parachute's fabric design.
出处 《产业用纺织品》 北大核心 2008年第8期22-25,共4页 Technical Textiles
关键词 降落伞绸 透气性 BP人工神经网络 预测 parachute fabric, air permeability, BP neural network, and prediction
  • 相关文献

参考文献7

二级参考文献21

  • 1朱炎 郭可谦.中国降落伞发展简述[C]..第一届中日机械技术史国际学术会议[C].北京,1998-10.441-446.
  • 2Kenneth J. Desabrais. Velocity Field Measurements in the Near Wake of a Parachute Canopy[ T ]. Doctor thesis of WORCESTER POLYTECHNIC INSTITUTE,April, 2002, 1~6
  • 3Movey D. F, Wolf D. F. Analysis of deployment and inflation of lardge ribbon parachute[J]. J. Aircraft 1974,11 (2): 96~ 103
  • 4S. E. Kunz. Analysis of initial parachute deployment dyring mass assault. [C]. AIAA-97-1451, 93~ 100
  • 5Peterson. C.W. and John D.W. Reduction in Parachute Drag due to Forebody Wake Effects [ J ]. AIAA Journal of Aircraft, 1983,20(1) :42~49
  • 6Wolf. D.F. A Coupling Apparent Mass for Parachute Inflation Equations. [ C ]. AIAA-89-0933. AIAA 10th Aerodynamic decelerator systems technology conference, Cocoa Beach, Florida,April 18-20, 1989
  • 7Hamid Johari. Aerodynamics of Parachute Opening [ R ]. AD Report. Mechanical Engineering Department Worcester Polytechnic Institute. Reporter number, 37594.6-E6, July 2002, 1 ~ 5
  • 8Vonce L. Behr, Walter P. Wolfe, Carl W. Peterson. An Overview of the Development of Vortex Based Inflation Code for Parachute Simulation [ C ]. 15th CEAS/AIAA Aerodynamic Decelerator Systems Technology Conference. June 1999, Toulouse, France
  • 9Jacques Blamont, Jack A. Jones. A New Method For Landing on Mars[J]. Acta Astronautic,2002,51(10) :723~726
  • 10Philip Schaefer, Alvin Derouen, S. Joseph Shane. An Acoustic Sensor For Triggering Parachute Decelerator Systems[J].AIAA2001-2035, 257~268

共引文献49

同被引文献41

引证文献5

二级引证文献12

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部