Volume 38 Issue 8
Aug.  2012
Turn off MathJax
Article Contents
Du Zheng, Wang Chaozhi. Main parameters of multi-purpose guided missile fuse and warhead optimization[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1022-1026. (in Chinese)
Citation: Du Zheng, Wang Chaozhi. Main parameters of multi-purpose guided missile fuse and warhead optimization[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1022-1026. (in Chinese)

Main parameters of multi-purpose guided missile fuse and warhead optimization

  • Received Date: 14 Jul 2011
  • Publish Date: 30 Aug 2012
  • For the current deficiencies of multi-purpose guided missile kill probability model against helicopter, the importance of vulnerability blade unit factors concept was introduced, laser fuse actuation model and warhead condition kill probability model of rotor blades were established by Monte Carlo method and kinetics theory with new ideas, which provided necessary mathematical tools for the accurate and objective analysis of multi-purpose guided missile kill probability against helicopter. Based on the establishment of multi-purpose guided missile kill probability model, the main parameters of multi-purpose guided missile fuse and warhead were optimized by multi-objective optimization. Results show that the single multi-purpose guided missile lethality performance and the parameters of fuse and war-head can improve significantly by the optimizing.

     

  • loading
  • [1]
    徐文旭,宋振铎,张更宇,等.多用途导弹战斗部对武装直升机终点毁伤建模及仿真[J].兵工学报,2007,28(6):671-676 Xu Wenxu,Song Zhenduo,Zhang Gengyu,et al.Research on terminal damage model and simulation of multi-purpose guided missile warhead attacking onhelicopter[J].Acta Armamentarii,2007,28(6):671-676(in Chinese)
    [2]
    牛冰,谷良贤,龚春林.破片战斗部对武装直升机目标的威力评估[J].弹道学报,2011,23(1):68-71 Niu Bing,Gu Liangxian,Gong Chunlin.Assessment of lethality of fragment warhead to armed-helicopter[J].Joumal of Ballistics,2011,23(1):68-71(in Chinese)
    [3]
    Srinivas J,Murthy B S N,Yang S H.Damage prediction of rotating blades using displacement residuals[J].Journal of Sound and Vibration,2008,316(1-5):25-31
    [4]
    Pawar P M,Ganguli R.On the effect of progressive damage on composite helicopter rotor system behavior[J].Composite Structures,2007,78(3):410-423
    [5]
    金光军,王朝志,陈万春.激光引信启动点的简化计算模型[J].战术导弹技术,2008(2):67—70 Jin Guangjun,Wang Chaozhi,Chen Wanchun.Simplified computation model of actuation point of laser fuze[J].Tactical Missile Technology,2008(2):67-70(in Chinese)
    [6]
    李廷杰.导弹武器系统的效能及其分析[M].北京:国防工业出版社,2000:188-210 Li Tingjie.Effectiveness analysis for missile weapon systems[M].Beijing:National Defence Industrial Press,2000:188-210(in Chinese)
    [7]
    过崇伟,郑时镜,郭振华.有翼导弹系统分析与设计[M].北京:北京航空航天大学出版社,2002:52-55 Guo Chongwei,Zheng Shijing,Guo Zhenhua.Analysis and design for winged missile system[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2002:52-55(in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(2292) PDF downloads(555) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return