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导弹
    Theory and Application Study on Underwater Trajectory Dynamic System Modeling of Submarine Launched Missile Carrier
    潜射导弹运载器水弹道动力系统建模及其应用研究
    Integrated Design of Integral Rocket-Ramjet Missile
    整体式冲压发动机导弹总体一体化设计
    Wavelet Application in Fault Diagnosis for Air Defense Missile
    小波理论在导弹故障诊断中的应用研究
    Method and Application of Winged Missile Oriented Multidisciplinary Robust Design Optimization
    面向飞航导弹的多学科稳健优化设计方法及应用
    The Research of BTT Missile Control System Based on Dynamic Inversion System and Neural Network Theory
    基于动态逆系统和神经网络理论的BTT导弹控制系统研究
    Study on Missile System-of-systems Combat Simulation Approach Based on SEB Composable Framework
    基于SEB组合框架的导弹体系对抗仿真方法研究
    Study on Sytem of Missile Sealifts with Wave Compensation for Navy Ships Connected Parallely
    舰艇并靠导弹补给及波浪补偿系统研究
    Research on Key Techniques of Guidance System of Stand-off Air to Surface Missile
    防区外空面导弹制导系统关键技术研究
    Infrared detection system for use in early stages of missile launching
    探测起始段导弹用的红外探测系统
    Missile Inertial Platform Self-alignment
    导弹惯性平台自对准
    Determination of Spin Angular Velocity for Spinning Missile
    自旋导弹弹体自旋角速度的确定
    Random Simulation of Sequential Probability Ratio Test for Spread of Impact Point of Missile
    导弹落点散布的序贯概率比(SPR)检验的随机模拟
    Induced Rolling Moment of Missile Wings for Tilt-wing and 《X-X》 Type Configuration at Supersonic Speeds
    超音速旋转弹翼式《X一X》型导弹弹翼部分的诱导滚转力矩
    IMPROVING THE MODEL OF KILL-PROBABILITY CALCULATION FOR THE MISSILE WITH CONTINUOUS BAR WARHEAD
    连续杆战斗部类导弹杀伤概率计算模型
    INDUCED ROLLING MOMENT ON WINGS OF A MISSILE WITH TILT-WINGS IN "X-X" CONFIGURATION AT SUPERSONIC SPEEDS
    超音速旋转弹翼式“X-X”型导弹弹翼部分的诱导滚转力矩
    OPTIMAL GUIDANCE LAW FOR THE MISSILE WITH BLIND AREA
    考虑制导盲区的导弹最优制导律
    THE MATHEMATIC MODEL OF THE HIT PROBABILITY AND KILL PROBABILITY OF A SINGLE ANTI-AICRAFT MISSILE WITH TOUCH INITIATION
    触发式防空导弹单发命中概率与单发杀伤概率数学模型
    Analysis of Missile Control System Stability with Monte Carlo Method
    用蒙特卡罗法分析导弹控制系统稳定性
    Application of Singular-Perturbation Method to Develop Missile Guidance Laws
    奇异扰动法在计算导弹导引规律中的应用
    DECOUPLING OF A KIND OF MISSILE CONTROL SYSTEM MODES
    一类导弹控制系统的模态解耦
 

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