1.
DETECTION PROBABILITY ANALYSIS OF PROJECTILE MISS DISTANCE FOR MILLIMETER WAVE PHASED ARRAY RADAR
毫米波相控阵雷达弹丸脱靶量检测概率分析
2.
Velocity Measuring System for Flying Projectiles Based on Light Meshs
基于光网靶的弹丸速度精确测量系统
3.
Miss Distance Analysis in APN Guided Radar Homing Missiles
采用修正比例导引的雷达寻的导弹脱靶量研究
4.
Miss distance analysis for missiles with lateral jets and aerodynamic surfaces
直接侧向力与气动力复合控制导弹脱靶量分析
5.
And the received power of remote system for Fl 6 aeroplane, as anexample, is computed.
不同脱靶量和不同脱靶方位角时，弹目交会过程激光引信接收系统的接收功率。
6.
A Method of Removing the Outliers of Doppler Frequency and Estimating Missile Miss Distance
一种去除多普勒频率野值及估计导弹脱靶量的方法
7.
Miss Distance Analysis of Terminal Maneuver Penetration for Surpersonic Anti-Ship Missile Based on Adjoint Technique
基于伴随技术的超音速反舰导弹末端机动突防的脱靶量分析
8.
Using laser Raman scattering to measure fuel content in ICF shell
激光拉曼散射测量ICF靶丸燃料含量
9.
PERFORATION OF THIN METAL PLATES STRUCK BY CONICAL-NOSED PROJECTILES AT RELATIVELY LOW VELOCITIES
锥头弹丸低速撞击下薄金属靶板的穿透
10.
Numerical simulations of simulated EFP penetration into alumina ceramic/steel composite target
EFP模拟弹丸侵彻陶瓷复合靶的数值模拟研究
11.
Analysis of penetration process and failure characteristic of Mg-10Gd-2Y-0.5Zr alloy penetrated by spherical bullet
镁合金靶板在球形弹丸侵彻过程中的破坏分析
12.
Research of the Information Detecte Acquire Method Which the Projectile Flying the Target Based on Sky Screen Target
基于天幕靶的弹丸过靶信息探测提取方法的研究
13.
Analysis for Vertical Target Precision of APFSDS
尾翼稳定脱壳穿甲弹立靶密集度分析
14.
Miss distance data processing method is introduced in combination with actual range application.
结合实际靶场应用介绍了脱靶量数据处理方法;
15.
Theoretical and Numerical Study on Failure Modes of Metal Plates under Normal Impact by Conical-Nosed Projectiles
锥头弹丸正撞击下金属靶板破坏模式的理论和数值模拟研究
16.
The Design and Manufacture For the Miss Distance Vector Measurement Software System
脱靶矢量测量系统软件的设计与实现
17.
Combined Measuring Method and Simulation of Deviation on Target by CCD and MEMS
CCD与MEMS组合测量弹丸落点偏差的方法
18.
The Influence of the Projectile Configuration on the Aerodynamic Characteristics of APFSDS for M=4～6,
马赫数4到6时弹丸外形对尾翼式脱壳穿甲弹气动力特性的影响