A novel calculation and simulation method on missile killing effect

被引:1
|
作者
Hou, Libing [1 ]
Zhu, Jihong [1 ]
Shi, Heng [1 ]
Kuang, Minchi [1 ]
机构
[1] Tsinghua Univ, Dept Precis Instrument, Beijing 100084, Peoples R China
基金
中国国家自然科学基金;
关键词
Killing effect; fragmentation warhead; system simulation; dynamic modeling; spatial geometry;
D O I
10.1142/S179396232350006X
中图分类号
TP301 [理论、方法];
学科分类号
081202 ;
摘要
To accurately describe the killing effect of missiles especially dealing with the small or fast target, a new method for calculating the killing effect. of missiles is proposed in this paper. The missile and the target are divided into several basic geometries based on their shapes, and then the equations of these geometries are established in their local frame. The mass center motion equations of the target and the missile are determined in the light of their initial positions and velocities, respectively, and every geometry moves with its center of mass according to its attitude. The equations of the fuze view field and the target can confirm whether the fuze detects the target, and whether the fragment hit the target can be certified by the same approach. This paper also writes a MATLAB simulation program for this calculation method and designs a new algorithm to determine the position relationship of space geometry using existing functions, and the simulation verifies the effectiveness of this method.
引用
收藏
页数:15
相关论文
共 50 条
  • [1] Research on Simulation Method of Missile Adapter's Separation Based on Combined Calculation
    Chen, Miao
    Jiang, Yi
    Shi, Shaoyan
    Zeng, Wei
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2019, 2019
  • [2] Calculation model for killing probability of fragmentation warhead of missile to air target
    Aerospace Technology and Material Engineering Institute, National University of Defense Technology, Changsha 410073, China
    Dandao Xuebao, 2006, 1 (45-47):
  • [3] Visual simulation of a missile killing an air target based on SIMBOX
    Zhang, Minghuan
    Gao, Ke
    Zhang, Ke
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2011, 29 (02): : 223 - 227
  • [4] Storage reliability calculation method for a certain missile
    Wu, Jinhuang
    Xu, Demin
    Song, Guibao
    Liu, Jimin
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2008, 26 (03): : 288 - 291
  • [5] Numerical calculation and simulation of missile jet-airplane interaction
    Wang Zhi
    Zeng Feipeng
    ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS, 2007, : 5142 - 5145
  • [6] A novel scheduling method for missile VRP
    Lai, Zefeng
    Ling, Qiang
    PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 2076 - 2081
  • [7] Study on hierarchical simulation experiment method for missile engagement simulation
    Wang, L
    Yang, F
    Wang, WP
    Zhu, YF
    System Simulation and Scientific Computing, Vols 1 and 2, Proceedings, 2005, : 342 - 346
  • [8] The numerical calculation method of simulating high accurately the missile jet
    Zeng, FP
    ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 4707 - 4709
  • [9] A Calculation Method of Kill Probability for Air-to-air Missile
    Lei, Hongli
    Hu, Zhaohui
    2012 FIFTH INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL INTELLIGENCE AND DESIGN (ISCID 2012), VOL 1, 2012, : 250 - 253
  • [10] Numerical simulation of the effect of wind on the missile motion
    Zyluk, Andrzej (andrzej.zyluk@itwl.pl), 1600, Polish Society of Theoretical and Allied Mechanics (52):