高超声速飞行器的弹道优化评估方法
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:

国家自然科学基金资助项目(61075001)


Evaluation method for hypersonic vehicle  trajectory optimization
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    高超声速飞行器弹道优化算法的综合评估对选取最优的弹道优化算法具有重要的参考意义。根据高超声速飞行器的特性,将其弹道分解为上升段、巡航段及俯冲段三个阶段,分别给出了各阶段的性能评价指标和对各阶段性能评价指标赋权的典型方法,并结合灰色关联度分析理论提出了弹道优化算法的综合评估方法。评估实例表明,该方法能定量地对多种弹道优化方法所生成的弹道进行综合性能评估,并能对备选优化方法的优劣进行排序。

    Abstract:

    Comprehensive evaluation for hypersonic vehicle trajectory optimization algorithm has good reference value on selecting optimal trajectory optimization algorithm. According to the features of hypersonic vehicle, trajectory was decomposed into ascent, cruise and descent stages; the performance evaluation indices of each stage and the typical methods of weighting for performance evaluation index were given respectively. Combining with the analysis theory of grey correlation degree, a comprehensive evaluation method of trajectory optimization algorithm was proposed. The calculation results show that the method can quantitatively evaluate trajectories produced by trajectory optimization methods and sort the alternative optimization methods by merits.

    参考文献
    相似文献
    引证文献
引用本文

胡怀中,郭茹霜,宫厚娟,等.高超声速飞行器的弹道优化评估方法[J].国防科技大学学报,2015,37(2):117-120.
HU Huaizhong, GUO Rushuang, GONG Houjuan, et al. Evaluation method for hypersonic vehicle  trajectory optimization[J]. Journal of National University of Defense Technology,2015,37(2):117-120.

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2014-07-20
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2015-05-16
  • 出版日期:
文章二维码