地地弹道导弹射击精度评估与分析

在分析射击弹道的基础上,建立了射击精度评估的简化数学模型,针对某型导弹飞行弹道仿真数据进行射击精度评估,精度指标与仿真结果一致,满足射击要求.     

旋转弹丸空气动力特性数值解法

为提高在弹道计算和弹丸设计中弹丸空气动力系数精度,采用隐式LU算法求解N S方程并考虑代数湍流模型,在旋转物面边界条件下计算弹丸的阻力、升力、俯仰力矩、滚转阻尼力矩、马格努斯力和力矩。通过对美国T388等弹丸的气动力系数计算并与弹道靶试验数据进行比较,以及对某榴弹的气动力计算结果在弹道计算中进行应用分析,表明用数值模拟得到的旋转弹丸空气动力系数好于以前用工程方法给出的结果。     

基于改进差分进化算法的内弹道参数优化

火炮内弹道参数直接影响其计算结果,内弹道参数优化设计是内弹道分析计算的重要环节。基于经典内弹道计算模型,以火药内弹道计算中最为敏感的燃速指数及其燃速系数为设计参量,以最大膛压及弹丸初速的计算值与测试值一致性为目标,对差分进化算法群体的初始化、变异因子及变异模式进行了改进,对某型火炮的内弹道参数进行了优化计算。优化设计结果表明改进后的差分进化算法满足内弹道设计工程实践要求,为内弹道参数优化设计提供了一种有效的算法。     

应急航材配送网络需求缓冲策略设计

航空装备是空军武器装备的主体,做好航材保障工作对于充分发挥装备作战效能,确保装备的作战使用具有重要意义。描述了应急需求冲击条件下缓冲控制问题,建立了应急航材配送网络影响缓存因素模型,进而建立了完整的应急航材需求冲击的缓冲策略设计框架,并进行了应急航材缓存分配建模。分别采用BP-GA方法对应急航材需求进行测算;保噪正态分布进行了缓冲策略公式的推演,需求冲能模型进行了单个缓存分配,并结合算例说明了其有效性。     

中远程战术导弹预测命中点的计算

探讨了如何根据被动段反战术弹道导弹运动状态来计算其弹道根轨道参数和预测命中点的一般方法。     

圆柱形微带天线的复合材料设计

本文介绍了满足微带天线使用温度要求的聚合物基复合材料设计的方法与过程。按照这种方法,设计并制造了一批微带天线产品,经高低温测试,证明都符合设计要求。     

Deterrence under nuclear asymmetry: THAAD and the prospects for missile defense on the Korean peninsula

The 2016 decision to deploy Terminal High Altitude Area Defense (THAAD) to South Korea has generated multitude of intensely politicized issues and has proved highly controversial. This has made it challenging to alleviate, let alone clarify, points of analytical and policy tensions. We instead disaggregate and revisit two fundamental questions. One is whether THAAD could really defend South Korea from North Korean missiles. We challenge the conventional “qualified optimism” by giving analytical primacy to three countermeasures available to defeat THAAD–use of decoys, tumbling and spiral motion, and outnumbering. These countermeasures are relatively inexpensive to create but exceedingly difficult to offset. Second, we assess the optimal way to ensure South Korean national security against North Korean missiles. By examining the balance of capability and issues of credibility/commitment, we show that the U.S. extended deterrence by punishment remains plentiful and sufficiently credible even without enhancing the current defense capability.     

Coating processes towards selective laser sintering of energetic material composites

This research aims to contribute to the safe methodology for additive manufacturing (AM) of energetic materials. Coating formulation processes were investigated and evaluated to find a suitable method that may enable selective laser sintering (SLS) as the safe method for fabrication of high explosive (HE) compositions. For safety and convenience reasons, the concept demonstration was conducted using inert explosive simulants with properties quasi-similar to the real HE. Coating processes for simulant RDX-based microparticles by means of PCL and 3,4,5-trimethoxybenzaldehyde (as TNT simulant) are reported. These processes were evaluated for uniformity of coating the HE inert simulant particles with binder materials to facilitate the SLS as the adequate binding and fabrication method. Suspension system and single emulsion methods gave required particle near spherical morphology, size and uniform coating. The suspension process appears to be suitable for the SLS of HE mocks and potential formulation methods for active HE composites. The density is estimated to be comparable with the current HE compositions and plastic bonded explosives (PBXs) such as C4 and PE4, produced from traditional methods. The formulation method developed and understanding of the science behind the processes paves the way toward safe SLS of the active HE compositions and may open avenues for further research and development of munitions of the future.     

考虑地球非球形引力摄动影响的自由段弹道解析解

针对地球非球形引力摄动影响下的自由段弹道快速计算问题,在非正交坐标系内建立考虑J2项摄动的地球引力作用下的运动微分方程,在轨道坐标系内建立扰动引力作用下的运动微分方程,并计算天向扰动引力加速度对应的质量偏差,进而通过椭圆轨道以修正J2项摄动运动微分方程;在建立上述运动微分方程解析解的基础上,给出了地心坐标系内弹道飞行器位置和绝对速度的表达式,从而提出了J2项摄动引力和扰动引力作用下的自由段弹道解析计算方法。仿真分析表明:该方法具有较高的计算效率,落点位置偏差小于20 m,满足弹道飞行器高精度实时制导、轨迹预测等应用需求。     

穿甲子弹偏心入射陶瓷/钢复合靶板试验

设计并进行了7.62mm穿甲子弹侵彻陶瓷/低碳钢复合靶板的弹道试验,得到了极限速度及陶瓷锥底部半径等数据。分析了锥底半径与入射速度、面板及背板厚度的关系,着重分析了偏心入射时靶板的抗弹机理。结果表明:陶瓷锥可分为破碎区和粉碎区,粉碎区半径约为面板厚度与弹丸半径之和;当弹着点距离陶瓷面板边缘大于5mm时,靶板的抗弹性能变化不大,而弹着点位于距陶瓷面板边缘小于5mm的板边区时,抗弹性能明显降低,靶板的有效防护面积应扣除板边区。