期刊文献+

基于遗传算法与人工神经网络相结合的固体推进剂燃速计算 被引量:5

Calculate for burning rate of solid propellant based on combination of genetic algorithm and back-propagation neural networks
原文传递
导出
摘要 为了提高固体推进剂燃速预示精度,将遗传算法(Genetic Algorithm)与误差反传(Back Propagation)网络结构模型相结合,设计了用遗传算法优化神经网络权重的新方法。以固体推进剂燃速数据库为基础,对推进剂的燃速进行了预估,并与BP算法进行了比较。结果显示,预估值与实际值接近,误差小于BP算法模型,具有良好的预示效果,为推进剂燃速预估提供了新方法。 In order to improve predicting precision of burning-rate of solid propellant. Combine Genetic Algorithm and Back-Propagation neural network, A fresh method on optimizing biases and weights of neural networks by Genetic Algorithm was demonstrated. Based on the database of solid propellants. Burning rate of solid propellant was predicted and contrasted to BP. The result showed that calculations were corresponding to practice and the errors were smaller than BP. So it supplies a new method for predicting burning rate of solid propellant.
出处 《计算机与应用化学》 CAS CSCD 北大核心 2006年第7期639-642,共4页 Computers and Applied Chemistry
关键词 推进剂燃速预估 遗传算法 神经网络 predicting of burning rate of solid propellant, genetic algorithm, neural network
  • 相关文献

参考文献14

  • 1Hechi Nielsen R. Theory of the back propagation neural network.Int J Conf On Neural Network, 1989, ( 1 ) :593 - 605.
  • 2Bornholdt A. General asymmetric neural network and structure design by genetic algorithms. Neural Network, 1992, 5 (2) : 327 -334.
  • 3Li Minqiang, Xu Boyi and Kou Jisong. Combination of genetic algorithm and back-propagation neural network. Theory and Practice of Systems Engineering, 1999, (2) :65 - 69.
  • 4Summerfield M, Sutherland GS, Webb WJ, Taback HJ and Hall KP. The burning mechanism of ammonium perchlorate propellants.ARS Progress in Astronautics and Rocketry Vol. 1 : Solid Propellant Rocket Research. New York : Academic, 1960 : 141 - 182.
  • 5Hermance CE. A model of composite propellant combustion including surface heterogeneity and heat generation. AIAA Journal,1966, 4(9) :1629 -1637.
  • 6Boggs TL, Derr RL and Beckstead MW. Surface structure of ammonium perchlorate composite propellants. AIAA Journal, 1970, 8(2) :370 -372.
  • 7Beckstead MW, Derr RL and Price CE. Model of composite solid-propellant combustion based on multiple flames. AIAA Journal,1970, 8(12) :2200 - 2207.
  • 8Glick RL and Condon JA. Statistical analysis of polydisperse heterpgeneous propellant combustion steady state. Thirteenth JANNAF Combustion Meeting, CPIA Publicatiaon 281, 1976.
  • 9King MK. Analytical and experimental study of the erosive burning of composite propellants. AD/A 050333, 1977.
  • 10King MK. A model for steady-state combustion of unimodal composite solid propellants. AIAA Paper, 78 -216.

共引文献22

同被引文献28

引证文献5

二级引证文献19

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