Volume 39 Issue 8
Aug.  2013
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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)

Design parameters sensitivity analysis of aircraft survivability

  • Received Date: 14 Sep 2012
  • Rev Recd Date: 02 Jul 2013
  • Publish Date: 30 Aug 2013
  • Since parameters sensitivity analysis can analyse the effects of design parameters on aircraft survivability more in-depth, the method of applying sensitivity analysis to aircraft survivability design was studied. The calculation model of aircraft survivability was established based on the model of aircraft susceptivity、vulnerability and combat capability. The parameters sensitivity analysis was divided into two cases of the modified design of the old aircraft and the program design of new aircraft, which provided the basis for the selection of parameters in the modified design and initial range reduction of design parameters in the program design. Simulation results show that the method is effective and feasible.

     

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