热真空条件下工作的电气电缆载流量计算与试验

高空制导飞行器从母舱释放后,制导舱与仪器舱之间部分电气电缆处于热真空条件下工作。对此种特定条件下的电缆进行了载流量计算。理论计算表明,给定的电缆设计满足在热真空条件下正常工作要求。最后简略介绍了载流量试验。     

导弹大攻角高机动飞行特性分析与仿真

以新一代无翼式气动布局导弹为背景,在大攻角气动特性理论基础上,分析了在导弹主动段、攻角在180°范围内变化的导弹飞行特性,得出了90°内大攻角最大转弯能力和180°攻角附近最大降速效果的结论。进行了俯仰平面S型轨迹机动飞行仿真,仿真结果说明了大攻角飞行的高机动特性。     

基于目标特征的光学遥感图像舰船检测方法

针对在大场景、高分辨率的光学遥感图像舰船目标检测中,传统的阈值检测方法效果不佳,而恒虚警法计算量大的缺点,研究一种根据检测舰船目标的特征,对每个可能的目标区域,快速计算检测阈值的方法。同时,研究基于RNN网络及信噪比的特征选择方法,对目标的特征进行优选并对候选目标进行鉴别。实验结果表明,采用本文方法进行舰船目标检测能获得较好的检测结果.     

基于以太环网的舰载网络设计技术

在对国外舰载网络发展分析后,结合舰载网络发展的军事需求,提出了基于以太网环网构建舰载高可靠网络的发展思路,并探讨了基于以太环网的舰载网络的体系结构、舰载多业务接入等相关技术。最后,利用三台万兆交换机搭建了单环网络测试环境,测试结果表明,以太环网的保护及恢复时间满足舰载网络的可靠性要求,基于以太环网的舰载网络设计方案可行。     

Recent advances in the synthesis and energetic properties of potassium-based potential green primary explosives

Primary explosives are utilized as a reliable initiator for secondary explosives in an extensive range of military and civilian operations. Heavy–metal–based primary explosives are moderate performing, more sensitive, and environmentally hazardous, posing a direct and indirect threat to health and safety. Therefore, heavy–metal–based primaries have been replaced by environment-friendly metal-based primary explosives, such as potassium complexes. This review presents not only a summary of the current progress of new-generation potassium-based primary explosives and their methods of preparation, energetic properties, and applications, but also a further comparison with traditional primary explosives. In addition, this work discusses the necessity of heavy metal–free primary explosives and the major challenges faced in replacing traditional primary explosives.     

Formation of adiabatic shearing band for high-strength Ti-5553 alloy: A dramatic thermoplastic microstructural evolution

By using split Hopkinson pressure bar, optical microscopy and electronic microscopy, we investigate the influence of initial microstructures on the adiabatic shear behavior of high-strength Ti–5Al–5V–5Mo–3Cr (Ti-5553) alloy with lamellar microstructure and bimodal microstructure. Lamellar alloy tends to form adiabatic shearing band (ASB) at low compression strain, while bimodal alloy is considerably ASB-resistant. Comparing with the initial microstructure of Ti-5553 alloy, we find that the microstructure of the ASB changes dramatically. Adiabatic shear of lamellar Ti-5553 alloy not only results in the formation of recrystallized β nano-grains within the ASB, but also leads to the chemical redistribution of the alloying elements such as Al, V, Cr and Mo. As a result, the alloying elements distribute evenly in the ASB. In contrast, the dramatic adiabatic shear of bimodal alloy might give rise to the complete lamination of the globular primary α grain and the equiaxial prior β grain, which is accompanied by the dynamic recrystallization of α lamellae and β lamellae. As a result, ASB of bimodal alloy is composed of α/β nano-multilayers. Chemical redistribution does not occur in ASB of bimodal alloy. Bimodal Ti-5553 alloy should be a promising candidate for high performance armors with high mass efficiency due to the processes high dynamic flow stress and excellent ASB-resistance.     

Deconsolidation and combustion performance of thermally consolidated propellants deterred by multi-layers coating

Both heating and solvent-spray methods are used to consolidate the standard grains of double-base oblate sphere propellants plasticized with triethyleneglycol dinitrate (TEGDN) (TEGDN propellants) to high density propellants. The obtained consolidated propellants are deterred and coated with the slow burning multi-layer coating. The maximum compaction density of deterred and coated consolidated propellants can reach up to 1.39 g/cm³. Their mechanic, deconsolidation and combustion performances are tested by the materials test machine, interrupted burning set-up and closed vessel, respectively. The static compression strength of consolidated propellants deterred by multi-layer coating increases significantly to 18 MPa, indicating that they can be applied in most circumstances of charge service. And the samples are easy to deconsolidate in the interrupted burning test. Furthermore, the closed bomb burning curves of the samples indicate a two-stage combustion phenomenon under the condition of certain thickness of coated multi-layers. After the outer deterred multi-layer coating of consolidated samples is finished burning, the inner consolidated propellants continue to burn and breakup into aggregates and grains. The high burning progressivity can be carefully obtained by the smart control of deconsolidation process and duration of consolidated propellants. The preliminary results of consolidated propellants show that a rapid deconsolidation process at higher deconsolidation pressure is presented in the dynamic vivacity curves of closed bomb test. Higher density and higher macro progressivity of consolidated propellants can be obtained by the techniques in this paper.     

基于HLA的维修保障仿真系统设计研究

针对作战单元维修保障能力评估的需求,提出建立基于HLA的维修保障仿真分析平台。在分析维修保障系统构成和运行过程的基础上,阐述了仿真联邦的设计思想和构建方法,并进行了系统设计。根据实际系统的运行逻辑开发了联邦剧情,基于HLA的开发和执行过程模型构建了联邦系统框架,设计了联邦对象模型,并指出了仿真实现的关键技术所在。     

RTI测试研究

运行支撑系统(RTI)作为应用高层体系结构(HLA)进行分布仿真的支撑系统,是实现HLA的核心。RTI的功能和性能直接关系到HLA仿真系统开发与应用的成败。首先阐述了RTI测试的内容和指标,接着结合例子详细研究了RTI测试的方法,最后对RTI测试研究进行了总结,为提高基于HLA的分布交互仿真系统的质量及可信度提供了基础。     

HLA联邦的桥接扩展和影响时空一致性的实例分析

随着计算机技术和仿真应用的发展 ,越来越需要组建大规模分布仿真系统 ,HLA框架的定义和应用为此提供了很好的契机。使用桥接技术把不同的联邦连接起来是构建大规模联邦的有效方法 ,其中桥接邦元更适合于不同RTI的异地连接。桥接HLA联邦会带来影响系统时空一致性和性能的新问题 ,时间推进和所有权转移是两个有代表性的例子 ,需要重点解决