[1] 肖元星.地面防空武器系统效费分析[M].北京:国防工业出版社,2006:1-2,218-219. XIAO Yuan-xing. Effectiveness-cost analysis of land-based air defense weapon system [M]. Beijing: National Defense Industry Press, 2006: 1-2, 218-219. (in Chinese) [2] 张学锋.火箭武器防空反导效能研究与系统仿真[D].南京:南京理工大学, 2006. ZHANG Xue-feng. Simulation research on damage probability of multiple launch rocket system intercepting aircraft [D]. Nanjing:Nanjing University of Scienceand Technology, 2006. (in Chinese) [3] 李铁鹏,乔相信,于锋,等.定向驱动预制破片战斗部数值模拟与试验[J].弹箭与制导学报,2013,33(1):89-92. LI Tie-peng, QIAO Xiang-xin, YU Feng, et al. Numerical simulation and experiment of directional driving preformed fragment warhead [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(1): 89-92. (in Chinese) [4] 石志彬,高敏,杨锁昌,等.瞄准式战斗部杀伤装置结构设计研究[J].兵工学报,2011,28(3):373-377. SHI Zhi-bin, GAO Min, YANG Suo-chang, et al. Research on the structural design of gimbaled warhead killing device [J]. Acta Armamentarii, 2011, 28(3): 373-377.(in Chinese) [5] 胡健,马大为,姚建勇,等.基于混沌神经网络的防空火箭炮交流伺服系统状态预测研究[J].兵工学报,2015,36(2):220-226. HU Jian, MA Da-wei, YAO Jian-yong, et al. State forecasting research of air-defense rocket launcher AC servo system based on chaotic neural network [J]. Acta Armamentarii, 2015, 36(2): 220-226. (in Chinese) [6] 杨勇,吕席卷.防空火箭弹对无人机毁伤概率评估模型[J].弹箭与制导学报,2014,34(6):87-90. YANG Yon, LYU Xi-juan. Damage probability assessment model of air defense rocket for UAV [J]. Journal of Projectiles, Rockets, Missiles and Guiolance, 2014, 34(6): 87-90. (in Chinese) [7] Zhang X F, Zhang Y X. Simulation research on damage efficiency of multiple launch rockets intercepting aircraft [J]. World Journal of Modeling and Simulation, 2008, 4(4): 312-318. [8] 李魁武.现代自行高炮武器系统总体技术[M].北京:国防工业出版社,2012: 358-359, 388. LI Kui-wu.Overall technology of modern antiaircraft weapon system[M]. Beijing: National Defense Industry Press, 2012: 358-359, 388. (in Chinese) [9] 王金云,王孟军,纪政.某型火箭弹对巡航导弹毁伤概率仿真分析[J].指挥控制与仿真,2012,34(1):92-95. WANG Jin-yun, WANG Meng-jun, JI Zheng. Simulation analysis on damage probability of rocket intercepting cruise missile [J]. Command Control & Simulation, 2012, 34(1): 92-95. (in Chinese) |