A novel launch dynamics measurement system for multiple launch rocket system and comparative analysis with numerical simulations

In this paper,a novel launch dynamics measurement system based on the photoelectric sensor pair is built.The actual muzzle time(i.e.a time duration that originates from the initial movement to the rocket's departure from the muzzle)and the muzzle velocity are measured.Compared with the classical methods,the actual muzzle time is obtained by eliminating the ignition delay.The comparative analysis method is proposed with numerical simulations established by the transfer matrix method for multibody systems.The experiment results indicate that the proposed measurement system can effectively measure the actual muzzle time and reduce the error of classical methods,which match well with the simulation results showing the launch dynamics model is reliable and helpful for further analysis and design of the MLRS.     

基于案例决策的地面无人装备编组评估方法

为解决地面无人装备编组评估问题,基于案例决策理论的思想,设计了地面无人装备编组方案评估的具体流程与方法,提出了"任务-编组-效能"的案例表示方法,分别定义了作战任务、编组方案及作战效能的规范化描述形式;在案例分析中,设计采用与数据属性相匹配的相似度计算方法,提取出相似案例,完成对备选方案的评估,为后续军事专家对编组方案的调整提供有效支撑.     

纳米SiO2改性聚合物锂离子电池的研究

研究了一种基于含氟聚合物的聚合物锂离子电池,考察了SiO2纳米粉对聚合物电解质隔膜的机械性能、吸液量以及电导率的影响,用电镜分析探讨了纳米改性聚合物电解质膜的微观结构;并以此纳米改性聚合物隔膜组装了小型的聚合物锂电池,研究了其电性能.     

磁绝缘传输线阴极准直建模与仿真

大型脉冲功率装置的磁绝缘传输线(Magnetically Insulated Transmission Line,MITL)阴极长度可达十余米,在悬臂结构下由于重力引起的末端挠度变形将达数厘米.如果不进行准直,由此造成的阴阳极间隙误差可能引起较明显的电流损失.借鉴HermesⅢ装置基于倾斜垫片的直线度调节方案,设计了用...