基于GA-ML-PMHT的多基站无源协同定位方法

针对无源协同定位系统中低可观测目标的航迹初始及维持问题,提出一种基于遗传算法的极大似然概率多假设的多基站无源协同定位方法。首先,建立多基站无源协同定位系统数学模型。其次,提出基于极大似然概率多假设的无源协同定位航迹初始算法,并首次利用遗传算法解决极大似然概率多假设中的优化求解问题,以提高目标检测跟踪性能。最后,通过滑窗法实现航迹维持。仿真结果表明,所提方法能够有效解决多基站无源协同定位系统中低可观测目标的航迹初始及维持问题。     

国有军工集团生产与创新双效率研究

文章利用DEA方法对2015-2016年我国国有军工集团的生产效率和创新效率进行了分析,结果发现:我国国有军工集团的生产效率在近两年整体上有所提升,受行业影响小于自身因素影响,受管理、技术等水平的影响与来自规模因素的影响相差不大;创新效率在近两年整体上有所下降,受行业影响与自身因素影响均较大,无效率主要来自创新管理水平或技术条件的不足;生产效率与创新效率呈现统计上不显著的正相关关系。在此基础上,提出了军工集团实施国企改革的几点建议,以供有关方面参考。     

单摄像机三维视觉技术

本文针对装配机器人的实际应用情况,提出了一种利用激光结构光提供的空间几何信息和图象中包含的物体表面与物体形状的信息来综合分析与提取空间物体的三维信息的方法。该方法已经实际应用于GKD-1型机器人视觉系统中。     

物元理论在优选对地打击目标中的应用

优选对地打击目标是现代信息化战争条件下联合作战对地火力协调中心在计划火力时的首要任务。旨在从目标的重要性、可靠性、射击紧迫性及对其射击时自身被发现的机会四个因素入手,举例证明如何构造物元模型,做到定性与定量相结合,对于编制炮兵C4I系统计划火力软件具有一定的参考价值。     

离散搜索力的最优配置模型及增量搜索计划

目前,离散搜索正越来越普遍地应用于各种搜索实践。为了优化搜索过程,提高离散搜索的效率,应用最优搜索理论,导出了待搜目标服从均匀分布、正态分布时离散搜索力的最优配置模型、目标的踪迹预测方法和最优增量搜索计划的求法,并通过实例作了演示,上述结论和方法为离散搜索力如何实施最优搜索提供了一定的理论依据。     

Bi‐objective missile rescheduling for a naval task group with dynamic disruptions

This paper considers the rescheduling of surface‐to‐air missiles (SAMs) for a naval task group (TG), where a set of SAMs have already been scheduled to intercept a set of anti‐ship missiles (ASMs). In missile defense, the initial engagement schedule is developed according to the initial state of the defensive and attacking units. However, unforeseen events may arise during the engagement, creating a dynamic environment to be handled, and making the initial schedule infeasible or inefficient. In this study, the initial engagement schedule of a TG is assumed to be disrupted by the occurrence of a destroyed ASM, the breakdown of a SAM system, or an incoming new target ASM. To produce an updated schedule, a new biobjective mathematical model is formulated that maximizes the no‐leaker probability value for the TG and minimizes the total deviation from the initial schedule. With the problem shown to be NP‐hard, some special cases are presented that can be solved in polynomial time. We solve small size problems by the augmented ? ‐ constraint method and propose heuristic procedures to generate a set of nondominated solutions for larger problems. The results are presented for different size problems and the total effectiveness of the model is evaluated.     

溅板式层板喷注单元燃烧特性数值分析

为了获得喷注单元结构参数对喷注器燃烧特性的影响规律,利用数值分析方法对单喷嘴溅板式层板喷注单元气-气燃烧特性进行研究,考察燃烧室特征长度及出口层喷嘴宽度对气氧/甲烷流动及燃烧特性的影响。在求解气-气燃烧流场方面,采用带化学反应的湍流N-S方程进行描述,其中化学动力学反应模型采用简化的单步9组分模型。研究结果表明:燃烧室特征长度的增大有利于特征速度效率的增加;该条件下采用溅板式层板喷注单元所对应的燃烧室特征长度约为600 mm。对比分析发现,出口层喷嘴宽度取0.15 mm时,水组分摩尔分数与热力计算值差别最大;当其值取1.05 mm时,燃烧室头部区域截面温度上升最快,取0.45 mm时上升最慢。总的来说,出口层喷嘴宽度取0.75 mm时,燃烧长度最短,燃烧效率最大。     

利用复单脉冲比的平面阵列雷达群目标检测方法

针对平面阵列雷达群目标检测问题,以矩形阵为例,详细分析方位向和俯仰向复单脉冲比虚部的统计特性;建立平面阵列雷达群目标检测模型,根据恒虚警检测原理推导复单脉冲比虚部的椭圆判决域,并利用复单脉冲比实部辅助判决,综合提出基于复单脉冲比的平面阵列雷达群目标检测算法。针对双目标情形进行仿真实验,结果表明:在较高信噪比、较大角度间隔以及幅度相当且相位差较大的条件下算法能够有效检测群目标。     

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。     

Air power in humanitarian intervention: Kosovo and Libya in comparative perspective

It would be hard to overstate the importance of air power in humanitarian intervention (HI) and the Responsibility to Protect (R2P). Yet, the role of air power in HI and R2P has been understudied. This article seeks to remedy the lack of systematic investigation. It does so by developing a framework for assessing the effectiveness of air power during military operations in HI and R2P and applies it to NATO’s air campaigns in Kosovo (Operation Allied Force) and Libya (Operation Unified Protector). Upon examination NATO is revealed to have fared better in Libya than Kosovo in positively accomplishing its stated humanitarian objectives, minimizing collateral damage and reducing the costs for the interveners, all of which are aspects considered by the model. The relative effectiveness of Operations Unified Protector is generally attributed to geography, diplomacy and technology. It is argued that better ground support, unmanned aerial vehicles (UAVs) and burden sharing are needed to enhance the utility of air power in HI and R2P even further.