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飞机作战生存力设计参数灵敏度分析

杨哲 李曙林 周莉 石晓朋

杨哲, 李曙林, 周莉, 等 . 飞机作战生存力设计参数灵敏度分析[J]. 北京航空航天大学学报, 2013, 39(8): 1096-1101,1121.
引用本文: 杨哲, 李曙林, 周莉, 等 . 飞机作战生存力设计参数灵敏度分析[J]. 北京航空航天大学学报, 2013, 39(8): 1096-1101,1121.
Yang Zhe, Li Shulin, Zhou Li, et al. Design parameters sensitivity analysis of aircraft survivability[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(8): 1096-1101,1121. (in Chinese)
Citation: Yang Zhe, Li Shulin, Zhou Li, et al. Design parameters sensitivity analysis of aircraft survivability[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(8): 1096-1101,1121. (in Chinese)

飞机作战生存力设计参数灵敏度分析

基金项目: 国家863计划资助项目(2009AA04Z406); 国家自然科学基金资助项目(61172083)
详细信息
  • 中图分类号: V221

Design parameters sensitivity analysis of aircraft survivability

  • 摘要: 针对灵敏度分析可以更深入地分析设计参数对飞机生存力的影响变化,研究了将灵敏度分析应用到飞机生存力设计的方法.基于飞机敏感性、易损性和作战能力模型建立了飞机生存力计算模型,分为旧机改型设计和新机方案设计两种情况对设计参数进行了灵敏度分析,为旧机改型设计中待改进参数的选取和新机方案设计中设计变量初始范围的缩减提供了依据.仿真实验及结果分析表明了文中方法的可行性.

     

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出版历程
  • 收稿日期:  2012-09-14
  • 修回日期:  2013-07-02
  • 网络出版日期:  2013-08-30

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