[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2017 , Vol. 37 >Issue 3: 31 - 34

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2017.03.009

PROJECTILES TECHNOLOGY

Sensibility Analysis of Firing Data of Anti-aircraft Gun Effecting onKill Probability of Fighter by Computer Simulating

  • PENG Fengsheng ,
  • NING Wei ,
  • LIANG Yongyong
Expand
  • 1 Shaanxi University of Technology, Shaanxi Hanzhong 723000, China
    2 National Key Laboratory of Aerospace Flight Dynamics, NPU, Xi'an 710072, China

Received date: 2016-05-10

  Online published: 2025-05-28

Fold

Abstract

In order to analysis effects of firing data and other parameters of anti-aircraft gun(AAG) on kill probability of fight, the distance between gun and target, firing error of AAG, mean square deviation of random error of fire control device, mean square deviation of gun dispersion error, rate of fire, time of firing in bursts, kill probability of single shot hit projectile were chosen intentionally. The kill probabilities of one AAG were calculated respectively by computer simulation with typical firing data and F16 as the target on the condition of the seven variables. The results showed that the four former variables have descending negative correlation with the kill probability, and the latter three variables have increasing positive correlation with the kill probability. The conclusions based on the calculation and analysis can provide beneficial reference to AAG engineering practice.

Key words： anti-aircraft gun; kill probability; firing data; sensibility; computer simulating

Cite this article

PENG Fengsheng , NING Wei , LIANG Yongyong . Sensibility Analysis of Firing Data of Anti-aircraft Gun Effecting onKill Probability of Fighter by Computer Simulating[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017 , 37(3) : 31 -34 . DOI: 10.15892/j.cnki.djzdxb.2017.03.009

[an error occurred while processing this directive]

References

[1]
陶德进, 王军, 朱凯. 高炮武器系统毁伤概率计算的蒙特卡罗法[J]. 系统工程理论与实践, 2014. 34(1):268-272.
[2]
粟琛钧, 刘永峰, 刘亮,等. 自行高炮主从作战模式下火力毁伤效能分析[J]. 四川兵工学报, 2015. 36(5):79-82.
[3]
刘云龙, 卢昱, 陈立云,等. 基于蒙特卡洛的高炮射击毁歼概率仿真[J]. 信息技术, 2010. 34(10):51-54.
[4]
熊志昂, 乔华平. 关于小高炮对空连发射击精度指标与命中概率的探讨[J]. 火力与指挥控制, 1996. 21(1):63-65.
[5]
潘志刚, 王学军. 舰载小口径舰炮对空碰炸毁伤概率计算与分析[J]. 弹箭与制导学报, 2005. 25(4):354-356.
[6]
田棣华, 萧元星, 王向威,等. 高射武器系统效能分析[M]. 北京: 国防工业出版社, 1991:171-482.
[7]
彭峰生, 廖振强. 弹炮结合防空武器系统毁伤概率分析[J]. 火力与指挥控制, 2007. 32(3):62-64.
[8]
YANG W, HAMMOUDI MN, HERRMANN G, et al. Two-state dynamic gain scheduling control applied to an F16 aircraft model[J]. International Journal of Non-LinearMechanics, 2012. 47(10):1116-4123.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]