伪装指数与生存能力的关系模型及求解

建立了战场伪装与系统生存能力的定量关系模型, 用其可以解析地计算系统被发现概率; 同时, 根据生存能力指标可以实现伪装指数的分解与合成, 为战场建设的总体规划提供依据     

聚碳硅烷——沥青共混体流变性与纺丝研究

聚碳硅烷和沥青分别是转化ＳｉＣ纤维和碳纤维的先驱体,两者共混或共聚就可以得到一种新功能纤维──ＳｉＣ－Ｃ纤维的先驱体。该先驱体的可纺丝性直接与聚碳硅烷和沥青的性质相关,只有两组份的可纺丝温度区间交叉才可能得到可纺性好的聚碳硅烷──沥青共混先驱体。该研究结果对于制备ＳｉＣ－Ｃ纤维时选择组份材料和共混工艺有指导意义。     

谈机载火控雷达的电磁兼容问题

机载火控雷达受到的电磁干扰,按干扰传播途径可分为电容性耦合干扰、电磁辐射干扰、共阻抗感应干扰等类型。简要地叙述了电磁干扰的产生、危害,以及如何采取恰当的措施,使干扰减到最小程度,从而满足机载火控系统对雷达越来越高的电磁兼容要求。     

热图像与瞄准镜分划图像实时叠加处理系统研究

热像仪是夜战中用于观察和瞄准的重要装备,但目前装备的某些坦克和装甲车辆上的热像瞄准镜,本身并不具有瞄准分划,因而也就很难获取目标更多的信息,限制了对目标进行有效的瞄准射击:为了使其热像瞄准镜同样具有坦克微光瞄准镜所具有的功能,作者利用高速数字信号处理器ADsP21535开发评估板,研究设计了热图像和瞄准镜分划图像实时叠加处理系统,从而较好的解决上述问题.     

【专题】“无人系统自主性与智能化”专题编者按

地空协同无人系统作为新质跨域智能作战力量已成为世界强国开展军事技术竞争的前沿方向。本文首先总结了地空协同无人系统的概念、功能及发展目标,分析了世界主要国家制定的专项规划,从形成智能作战体系、改变战场攻防平衡及全面提高作战效能三个方面阐述了地空协同无人系统对未来战争的重大意义;其次,针对其面临的环境复杂、资源受限和平台异构等约束条件,从分布式态势认知、适应性智能导航及异构系统协同控制等方面总结了地空协同无人系统需要突破的关键技术;最后,为应对智能化战争挑战,从技术瓶颈、平台建设及政策支持等方面提出发展建议。该研究可为地空协同无人系统在国防科技领域的研究、应用和发展提供参考。     

高校智能无人系统运用人才队伍建设研究

智能无人系统是能够通过先进的技术进行操作或管理而不需要人工干预的人工系统,具有自主性、智能性以及人机耦合性等特征。随着科技快速更迭、国家战略支持、国家安全保障等要素驱动,高校智能无人系统运用人才队伍建设的研究势在必行。本文认为,当前,高校智能无人系统运用人才队伍呈现出愈发注重交叉学科研究、理论联系实践、开展专业认同教育以及课程思政建设等特点,这需要高校在引进和培育、交叉和融合以及专业化和高素质上下功夫,稳步推进高水平创新团队建设和一流专业学科群建设,同时稳步加大复合型人才培养力度,以为高校智能无人系统研发提供人才和智力保证。     

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.     

The deformation and failure mechanism of cylindrical shell and square plate with pre-formed holes under blast loading

The deformation and failure mechanism of cylindrical shells and square plate with pre-formed holes under blast loading were investigated numerically by employing the Ansys 17.0 and Ls-Dyna 971. To calibrate the numerical model, the experiments of square plates with pre-formed circle holes were modeled and the numerical results have a good agreement with the experiment data. The calibrated numerical model was used to study the deformation and failure mechanism of cylindrical shells with pre-formed circle holes subjected to blast loading. The structure response and stress field changing process has been divided into four specific stages and the deformation mechanism has been discussed systematically. The local and global deformation curves, degree of damage, change of stress status and failure modes of cylindrical shell and square plate with pre-formed circular holes are obtained, compared and analyzed, it can be concluded as: (1) The transition of tensile stress fields is due to the geometrical characteristic of pre-formed holes and cylindrical shell with arch configuration; (2) The existence of pre-formed holes not only lead to the increasing of stress concentration around the holes, but also release the stress concentration during whole response process; (3) There are three and two kinds of failure modes for square plate and cylindrical shell with pre-formed holes, respectively. and the standoff distance has a key influence on the forming location of the crack initiating point and the locus of crack propagation; (4) The square plate with pre-formed holes has a better performance than cylindrical shell on blast-resistant capability at a smaller standoff distance, while the influence of pre-formed holes on the reduction of blast-resistant capability of square plate is bigger than that of cylindrical shell.     

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.     

一种关于~pc(0≤c<1)的快精算法

求pc(p>1,正整数)的值时,若c较小,通常会存在收敛速度较慢以及数值字长有限所致精度变差的问题。提出了一种关于pc(0≤c<1)的快精算法,该方法按照定点二进制数特点,通过适当扩大c值,利用牛顿迭代法求取近似值,在采用选值法确定初值时,将对应值域分为若干等间隔子区间,初值精度取决于间隔h的大小,而h的大小则根据迭代精度和预定迭代次数确定,由此可获得高精度初值,从而在理论上使pc的迭代计算达到快速、高精度的目的。