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基于回归神经网络的非线性舰炮弹道偏差预测 被引量:1
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作者 马野 戴耀 汪德虎 《弹道学报》 CSCD 北大核心 2002年第3期22-25,31,共5页
提出一种基于回归神经网络及弹道机理模型对非线性弹道系统进行辩识的方法 ,通过观测上升段弹丸飞行轨迹 ,采用混合模型预测弹道的误差规律 ,最后估计出弹着点 ,对系统采用 MATLAB进行仿真 ,结果表明 ,该方法有效可行 .
关键词 回归神经网络 舰炮 弹道偏差 预测 弹道方程 非线性弹道
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Penetration of disk fragments following impact on thin plate 被引量:6
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作者 Juan-juan LI Hai-jun XUAN +2 位作者 Lian-fang LIAO Wei-rong HONG Rong-ren WU 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2009年第5期677-684,共8页
To investigate the ballistic resistance and failure pattern of aeroengine casing following the impact of disk fragments, and to determine the optimum case structure, the phenomena of a 1/3rd disk fragment impact on si... To investigate the ballistic resistance and failure pattern of aeroengine casing following the impact of disk fragments, and to determine the optimum case structure, the phenomena of a 1/3rd disk fragment impact on single and double-layered thin plate targets were simulated using nonlinear dynamical analysis software MSC.Dytran. Strain rate effect was introduced in a Johnson-Cook (JC) material model for the disk fragment and the plate. Impact modeling was based on the Arbitrary Lagrange-Eulerian method, and simulated using explicit finite element method (FEM). Simulation results showed that the major failure pattern of the plate is shearing and tensile fracture with large plastic deformation. It was also concluded that the ballistic limit velocity increases with the standoff distance when it is beyond a certain value, and that greater resistance is obtained when the front plate has either a proportionately low or high thickness. The impact resistance of a double-layered plate may exceed that of a single plate if the thicknesses and standoff distance of the two plates are set appropriately. 展开更多
关键词 AEROENGINE Disk burst failure Case containment capability Ballistic limit velocity
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