InSb纳米颗粒的制备与原子力显微镜

为进一步研究半导体纳米材料的物理特性,用真空沉积的方法在SiO2基片上制备了纳米InSb颗粒膜。用原子力显微镜扫描样品表面的分析显示,纳米InSb颗粒均匀地分布在SiO2基片表面。实验结果表明通过改变镀膜时间,可以得到具有不同颗粒尺寸的InSb纳米颗粒。     

一种具有抑风性能的综合火力/飞行控制系统

提出了飞机中性稳定的直接力控制模态。将这一模态应用于综合火力/飞行控制中的空-空机炮攻击,着重研究了中型稳定模态的抗垂风性能。此模态的应用实现了航迹基本不变的机身瞄准直接力控制,提高了抗垂风能力,明显地改善了姿态跟踪精度,延长了交火时间,并最终减小了脱靶量。     

兵力编成结构裁剪中指挥关系优化研究

由于决策个体控制战场作战平台资源实体,通过平台资源实体执行作战任务,作战平台资源实体在任务上的聚集导致决策个体间需要复杂的交互协作与交流,兵力编成需要为任务的执行创造良好的交互结构。基于任务执行的兵力编成包括两方面的内容:一是指控决策结点间的协作关系;二是指控决策结点间的指挥关系。本文基于决策个体在任务上的协作关系设计兵力编成的指挥关系,以最小化编成中总的协作工作负载为目标,并描述了编成指挥决策关系的生成过程,对生成过程的求解采用了优化协作树算法。     

巡航导弹(CM)作战有效度预测

以“沙漠之狐”、“沙漠风暴”行动为背景 ,对 CM的作战有效度作了预估 ,预估中用不同方法 ,对 CM的作战能力作了初步计算与分析。     

防空导弹武器系统反导效能指数描述方法模型

以防空导弹武器系统反TBM效能为研究对象 ,建立了防空导弹武器系统反TBM效能指数描述模型 ,并以方案A ,B ,THAAD(某中间方案 )为评价对象进行了实例计算 ,分析了评价结果 ,得出了结论。     

A generalized model for estimation of aerodynamic forces and moments for irregularly shaped bodies

A novel method for estimation of an aerodynamic force and moment acting on an irregularly shaped body (such as HE projectile fragments) during its flight through the atmosphere is presented. The model assumes that fragments can be approximated with a tri-axial ellipsoid that has continuous surface given as a mathematical function. The model was validated with CFD data for a tri-axial ellipsoid and verified using CFD data on aerodynamic forces and moments acting on an irregularly shaped fragment.The contribution of this method is that it represents a significant step toward a modeling that does not require a cumbersome CFD simulation results for estimation of fragment dynamic and kinematic parameters. Due to this advantage, the model can predict the fragment motion consuming a negligible time when compared to the corresponding time consumed by CFD simulations. Parametric representation (generalization) of the fragment geometrical data and the conditions provides the way to analyze various correlations and how parameters influence the dynamics of the fragment flight.     

Challenges of institutional coordination in complex defense acquisition programs: the case of the Republic of Korea’s F-X program

Decision-making in defense acquisition programs in the Republic of Korea (ROK) has been problematic, especially in highly advanced complex systems. The highly disputed force modernization program for the ROK Air Force’s fifth-generation fighter, dubbed the Fighter eXperiment, went through extreme turbulence during the type selection phase. The gist of the turbulence became evident through poor institutional coordination within the defense acquisition authorities that eventually forced them to rescind the decision generated from their own yearlong efforts, thus basically shooting themselves on the foot. The paper highlights the background of the program and reviews the institutional elements that influenced the decision-making process, and conclude that the absence of an effective coordination mechanism has made decision-making in complex defense programs even more troublesome.     

近期美国海军南海地区活动态势分析

随着南海地区力量结构和美对华战略的转变,南海地区成为中美战略博弈的焦点。为围堵遏制中国的崛起,美国针对中国在南海实施了一系列海上挑衅行为。美国海军作为美国军事干预的主要力量,从兵力部署、演习演训、“航行自由”行动等着手,积极拉拢域内外盟友,展开并强化了在南海地区的军事活动。这些军事活动表现出极强的针对性和实战性,致使中美海上摩擦和竞争加剧。未来,美国为维护主导的全球秩序,将进一步提升美国海军在南海地区的威慑力。美国海军会借助并增加域内盟友的军事力量,继续维持高强度的装备平台活动及“航行自由”行动,推动海上力量合作。     

直列式内燃机往复惯性力对瞬时转速影响的仿真研究

提出了两种由直列式内燃机往复惯性力计算转速波动的仿真模型 ,对不同气缸间惯性力的相位耦合进行了仿真分析 ,证明缸数对转速波动的幅度和频率均有着很大的影响 ;利用希尔伯特变换对转速波动信号进行时频分析 ,证明了多缸机转速波动波形为调频余弦曲线     

力的空间连续条件及应用研究

分析了力的空间不连续性 ,导出了力的空间连续条件 ,并结合实例提出了两种实现力值连续变化的轨道计算方法