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基于改进遗传算法的燃气轮机自适应建模

刘永葆 贺星 黄树红

刘永葆, 贺星, 黄树红. 基于改进遗传算法的燃气轮机自适应建模[J]. 航空动力学报, 2012, 27(3): 695-700.
引用本文: 刘永葆, 贺星, 黄树红. 基于改进遗传算法的燃气轮机自适应建模[J]. 航空动力学报, 2012, 27(3): 695-700.
LIU Yong-bao, HE Xing, HUANG Shu-hong. Adaptive simulation of gas turbine performance using improved genetic algorithm[J]. Journal of Aerospace Power, 2012, 27(3): 695-700.
Citation: LIU Yong-bao, HE Xing, HUANG Shu-hong. Adaptive simulation of gas turbine performance using improved genetic algorithm[J]. Journal of Aerospace Power, 2012, 27(3): 695-700.

基于改进遗传算法的燃气轮机自适应建模

基金项目: 国家自然科学基金创新研究群体科学基金(50721005)

Adaptive simulation of gas turbine performance using improved genetic algorithm

  • 摘要: 综合运用了一种改进的遗传算法和自适应建模技术对燃气轮机的精确特性进行寻优获取.引入自适应机制优化交叉和变异算子,同时引入模拟退火算法,使改进遗传算法能很快接近最优解,并能跳出局部最优的陷阱,在保证解的质量的同时提高了收敛的速度.针对以往自适应模型中未考虑测量参数间的线性相关性和不同的传感器测量精度对目标函数的影响等问题,采用加权方法建立了较为完备的燃气轮机自适应数学模型,应用改进遗传算法获取燃气轮机部件的精确特性,实例计算结果表明:模拟退化改进遗传算法进行的自适应建模效果更好.

     

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出版历程
  • 收稿日期:  2011-04-25
  • 修回日期:  2011-09-07
  • 刊出日期:  2012-03-28

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