巡航导弹群突防舰载反导系统快速分析模型

杜政; 王朝志; 陈万春

巡航导弹群突防舰载反导系统快速分析模型

北京航空航天大学宇航学院, 北京 100191

详细信息

中图分类号: TJ761.6
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出版历程
- 收稿日期: 2013-01-09
- 网络出版日期: 2013-11-30

Fast analytical model of cruise missiles penetration ship-based anti-missile system

School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 针对巡航导弹初始设计阶段需要频繁进行人机对话的特点，引入拦截弹拦截性能修正因子的概念，综合运用导弹分析方法中的估计方法与检验方法，以突防效率为评价指标采用新思路建立了巡航导弹群突防舰载反导系统快速分析模型，为初始设计阶段提高巡航导弹作战性能提供快速、可靠的数学工具.基于所建立的快速分析模型，对影响巡航导弹突防典型舰载反导系统的主要因素进行灵敏度分析，分析结果可为巡航导弹设计指明方向.
- 巡航导弹 /
- 拦截性能修正因子 /
- 突防效率 /
- 灵敏度分析
Abstract: Aim at the characteristics of frequent human-computer dialogue of cruise missile in the initial design phase, the interceptor performance correction factor was introduced, a fast analytical model of cruise missiles penetration ship-based anti-missile system with penetration efficiency as evaluation index was established with new ideas by the integrated use of estimation method and simulation method of missile analytical methods, which provided fast and reliable mathematical tools for the improvement of cruise missile operational performance in the initial design phase. Based on the establishment of fast analytical model, sensitivity analysis of the main factors that affect cruise missiles penetration typical ship-based anti-missile system were conducted. Results can set the direction for cruise missile design.
- cruise missile /
- interceptor performance correction factor /
- penetration efficiency /
- sensitivity analysis

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参考文献(11)

[1]	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, 2002:37-38 Guo Chongwei, Zheng Shijing, Guo Zhenhua.Analysis and design for winged missile system[M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2002:37-38 (in Chinese)
[2]	Yan Daiwei, Pan Lei, Gu Liangxian.Estimation the mission effectiveness of hypersonic cruise missile in conceptual design.AIAA-2008-176, 2008
[3]	孙学风, 赵彦辉, 于天顺.巡航导弹突破要地防空群多层防线的概率模型[J].兵工自动化, 2011, 30 (7):4-6 Sun Xuefeng, Zhao Yanhui, Yu Tianshun.Probabilistic model of cruise missile breaking through multiplayer defense of air defense group for strategic points[J].Ordnance Industry Automation, 2011, 30 (7):4-6 (in Chinese)
[4]	Yu Lei, Tang Shuo.Research on modeling and simulation of cruise missile interception system based on object-oriented petri Net[C]// 2010 3rd IEEE International Conference on Computer Science and Information Technology.Sichuan, China:IEEE, 2010:632-635
[5]	Mahafza R B, Elsherbeni Z A.Matlab simulations for radar systems design[M].New York:Chapman & Hall/CRC, 2004:118-122
[6]	许小剑, 黄培康.雷达系统及其信息处理[M].北京:电子工业出版社, 2010:145-168 Xu Xiaojian, Huang Peikang.Radar system and information processing[M].Beijing:Publishing House of Electronics Industry, 2010:145-168 (in Chinese)
[7]	邢昌风, 李敏勇, 吴玲.舰载武器系统效能分析[M].北京:国防工业出版社, 2008:104-106 Xing Changfeng, Li Minyong, Wu Ling.Effectiveness analysis for shipborne weapon system[M].Beijing:National Defence Industrial Press, 2008:104-106 (in Chinese)
[8]	刘小明, 周浩, 陈万春, 等.基于SIMULINK/RT-LAB的导弹制导系统HIL仿真平台设计[J].红外与激光工程, 2007, 36:366-369 Liu Xiaoming, Zhou Hao, Chen Wanchun, et al.Simulink/RT-LAB based HIL missile guidance system simulation platform research[J].Infrared and Laser Engineering, 2007, 36:366-369 (in Chinese)
[9]	薛定宇, 陈阳泉.高等应用数学问题的MATLAB求解[M].北京:清华大学出版社, 2005:284-286 Xue Dingyu, Chen Yangquan.Application of MATLAB in solving the higher mathematical problems[M].Beijing:Tsinghua University Press, 2005:284-286 (in Chinese)
[10]	Ökten G, Willyard M.Parameterization based on randomized quasi-Monte Carlo methods[J].Parallel Computing, 2010, 36 (7):415-422
[11]	刘含香.模糊数学理论及其应用[M].北京:科学出版社, 2012:12-14 Liu Hanxiang.The theory of fuzzy mathematics and application[M].Beijing:Science Press, 2012:12-14 (in Chinese)