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基于ADE-ELM的涡轴发动机建模方法

焦洋 李秋红 朱正琛 廖光煌

焦洋, 李秋红, 朱正琛, 廖光煌. 基于ADE-ELM的涡轴发动机建模方法[J]. 航空动力学报, 2016, 31(4): 965-973. doi: 10.13224/j.cnki.jasp.2016.04.025
引用本文: 焦洋, 李秋红, 朱正琛, 廖光煌. 基于ADE-ELM的涡轴发动机建模方法[J]. 航空动力学报, 2016, 31(4): 965-973. doi: 10.13224/j.cnki.jasp.2016.04.025
JIAO Yang, LI Qiu-hong, ZHU Zheng-chen, LIAO Guang-huang. Turbo-shaft engine modeling method based on ADE-ELM[J]. Journal of Aerospace Power, 2016, 31(4): 965-973. doi: 10.13224/j.cnki.jasp.2016.04.025
Citation: JIAO Yang, LI Qiu-hong, ZHU Zheng-chen, LIAO Guang-huang. Turbo-shaft engine modeling method based on ADE-ELM[J]. Journal of Aerospace Power, 2016, 31(4): 965-973. doi: 10.13224/j.cnki.jasp.2016.04.025

基于ADE-ELM的涡轴发动机建模方法

doi: 10.13224/j.cnki.jasp.2016.04.025
详细信息
    作者简介:

    焦洋(1991-),男,河北昌黎人,硕士生,从事航空发动机建模与仿真研究.

  • 中图分类号: V233.7

Turbo-shaft engine modeling method based on ADE-ELM

  • 摘要: 提出了基于自适应微分进化-极端学习机(ADE-ELM)求解平衡方程的高精度涡轴发动机实时部件级模型建立方法.基于牛顿-拉夫逊(N-R)迭代模型,以迭代计算前模型平衡方程残差为输入,迭代收敛后平衡方程猜值修正量为输出,训练极端学习机,并采用自适应微分进化(ADE)算法优化极端学习机(ELM)参数,提高猜值修正量映射精度.ADE算法中采用sigmoid型自适应缩放因子,提高了微分进化算法的寻优能力.在涡轴发动机不同飞行状态下的测试结果表明,以N-R迭代算法模型为基准,基于ADE-ELM的发动机模型,最大建模误差约为一次通过算法的1/3,运算耗时约为一次通过算法的1/3,验证了算法的有效性.

     

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出版历程
  • 收稿日期:  2014-08-27
  • 刊出日期:  2016-04-28

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