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    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
    The Mechanism and Effect on the Changes of Heat Shock Protein70, p38 Mitogen-Activated Protein Kinase in Missile Craniocerebral Injuries under High Temperature and High Humidity Environment
    高温高湿环境下颅脑火器伤后HSP70、p38 MAPK变化及其作用机理
    Study on the Optimal Allocation Policy of Tactical Missiles to Targets
    战术导弹对目标打击的最优分配策略研究
    Integrated Design of Integral Rocket-Ramjet Missile
    整体式冲压发动机导弹总体一体化设计
    Research on the Key Technologies of the Guidance System for Cruise Missile
    巡航导弹制导系统关键技术研究
    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
    The Study on the Control System of Aerodynamic Missile Based on Fractional Calculus
    基于分数阶微积分的飞航式导弹控制系统设计方法研究
    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
    Modal Test and Parameter Identification of a Flutter Wing Model with External Missiles
    机翼带外挂颤振模型模态试验与参数识别
    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
 

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