Sensitivity analysis of design parameters of an anti-aircraft gun for hit probability enhancement

被引:0
|
作者
Kang Park
Hwan-il Kang
Chong-man Kim
机构
[1] Myongji University,Department of Mechanical Engineering
[2] Myongji University,Department of Information and Communication
[3] Myongji University,Department of Industrial Engineering
关键词
Anti-aircraft gun; Hit probability; Sensitivity analysis; Sensor error;
D O I
暂无
中图分类号
学科分类号
摘要
To design an anti-aircraft gun with high hit-probability, the effect of each design parameter on the hit-probability needs to be estimated. For this purpose, the sensitivity analysis is widely used. However, the whole firing process of the anti-aircraft gun is too complicated to use the traditional sensitivity analysis that uses partial derivatives of the output function regarding the specific design parameter. The inaccuracy of the parts of the anti-aircraft gun that exists at different stage of the firing process will result in decrease of hit-probability. In this paper, the firing process of the anti-aircraft gun is described and each step of the firing process is formulated with the equation that includes the inaccuracies of parts. The anti-aircraft gun is modeled using the transformation matrix from design parameter to the traverse and the elevation angle considering inaccuracy of design parameters. Then by disturbing the each design parameter with random numbers whose average and standard deviation are known and calculating the resultant hit performance, the sensitivity of the design parameter on the hit probability can be estimated.
引用
收藏
页码:3043 / 3046
页数:3
相关论文
共 50 条
  • [21] Architecture Design of the Anti-Aircraft System Based on Architecture Framework
    Zhao, Qingsong
    Chen, Qihong
    Qian, Qunyou
    Zhao, Han
    2023 IEEE INTERNATIONAL SYSTEMS CONFERENCE, SYSCON, 2023,
  • [22] Test Method for Judging Kill Probability of Anti-aircraft Artillery by Quantity of Killed Targets
    Xie J.
    Wu J.
    Wang S.
    Fan Z.
    Han B.
    Binggong Xuebao/Acta Armamentarii, 2020, 41 (04): : 634 - 640
  • [23] The Analysis of the Anti-aircraft Missile Flight Controlled with Gyroscopic System
    Stefanski, Konrad
    SCIENTIFIC SESSION ON APPLIED MECHANICS X, 2019, 2077
  • [24] A Damage Probability Calculation Model Based on State Equation of Firing Error for Anti-Aircraft Artillery
    Wang X.
    Wang J.
    Xie J.
    Guo Z.
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2020, 54 (09): : 961 - 966
  • [25] Sensitivity Analysis for Design Parameters of Electric Tilt-Rotor Aircraft
    Wang, Yu
    Ma, Wenyuan
    Chen, Zhaolin
    AEROSPACE, 2024, 11 (04)
  • [26] Design of PID Controllers of Anti-aircraft Artillery Servo System with Multiple Performance Specifications
    李银伢
    盛安冬
    王远钢
    Journal of China Ordnance, 2007, (03) : 185 - 190
  • [27] Research on rigid-flexible coupling launch dynamics modeling method for a self-propelled anti-aircraft gun
    Zhang, Xin
    Wang, Baobao
    Zhang, Hui
    Yu, Cungui
    2021 8TH INTERNATIONAL FORUM ON ELECTRICAL ENGINEERING AND AUTOMATION, IFEEA, 2021, : 787 - 793
  • [28] Analysis and Countermeasures of Aimer Operation Errors of a Certain Type of Anti-aircraft Artillery
    Guo, Junlong
    Yang, Rongzhi
    Wang, Dapeng
    Liu, Zaochen
    PROCEEDINGS OF THE 15TH INTERNATIONAL CONFERENCE ON MAN-MACHINE-ENVIRONMENT SYSTEM ENGINEERING, 2015, 356 : 125 - 131
  • [29] An analysis of the gyroscope dynamics of an anti-aircraft missile launched from a mobile platform
    Koruba, Z.
    Krzysztofik, I.
    Dziopa, Z.
    BULLETIN OF THE POLISH ACADEMY OF SCIENCES-TECHNICAL SCIENCES, 2010, 58 (04) : 651 - 656
  • [30] The numerical analysis of dynamics and control of a gyroscopic scanning system in an anti-aircraft missile launcher
    Koruba, Zbigniew
    COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2011, 16 (05): : 2230 - 2236