1.
Analysis of Trajectory Simulation of Proportional Guidance Based on Matlab
基于Matlab的比例导引弹道仿真分析
2.
Performance of proportional navigation law for terminal laserguided projectile
激光末制导炮弹比例导引律性能研究
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.
A Method of Computer Simulation on Proportion Usher Related to Anti-vessel Missiles;
反舰导弹比例导引的一种计算机模拟仿真方法
5.
Investigation on Design of Homing Missile Strapdown Guidance System Based on Proportional Navigation Laws;
自寻的导弹捷联导引系统实现比例导引设计与研究
6.
Research on Robust Prediction of Fuze-warhead Coordination for ATBM
反弹道导弹引战配合的鲁棒预测研究
7.
Ultrasound-guided minimally invasive percutaneous nephrolithotomy pneumatic lithotripsy 174 cases of kidney stones
超声引导微创经皮肾穿刺气压弹道碎石治疗肾结石174例
8.
Minimally invasive percutaneous nephrolithotomy in the treatment of renal calculi under ultrasound guidance(report of 98 cases)
超声引导下微创经皮肾镜气压弹道治疗肾结石98例报告
9.
Pneumatic lithotripsy through percutaneous nephroscope under the guidance of color doppler ultrasound treating 9 cases of multiple renal calculi
彩超引导经皮肾镜气压弹道碎石术治疗多发肾结石9例效果研究
10.
ballistic, guided, nuclear, etc missiles
弹道、 制导、 核...导弹
11.
Studies of Guidance and Combined Control in Terminal Phase When Intercepting Tactical Ballistic Missile;
拦截战术弹道导弹末段导引和复合控制研究
12.
Comparative studies of interior ballistic performance among several missile eject power systems
几种导弹弹射动力系统内弹道性能比较
13.
Development of infrared imaging seeker simulation system and technologies for ballistic missile defense KKV
弹道导弹防御动能拦截弹红外成像导引头仿真系统与技术的发展
14.
In order to realize large airspace transfer orbital trajectory of an anti-ship missile, a 3-dimensional virtual target′s proportional navigation guidance(PNG) law is proposed.
为了实现反舰导弹的大空域变轨,提出了一种三维虚拟目标比例导引律。
15.
Analysis of an optimum atbm seeker fuze time-delay algorithm to burst the warhead
反战术弹道导弹引信炸点控制算法研究
16.
rocker ballistics
火箭[导弹]弹道学
17.
Detection Distance Estimation of Infrared Homing Head upon Tactical Ballistic Missile(TBM) in Midcourse Flight
红外导引头对中段战术弹道导弹目标的探测距离估算
18.
Optimum Design and Implementation of Initial Arc Trajectory for a Three-point Guidance Missile
三点法导引导弹初始段弧形弹道优化设计及实现