一种可实现TF/TA2的无人飞行器三维航迹规划方法

从规划空间的有效表达着手对无人飞行器三维航迹规划展开研究,基于地形和威胁提出的飞行器航迹规划方法将航迹规划分为学习阶段和查询阶段,环境信息和飞行器的大部分约束条件结合在路线图的构造过程中,航迹搜索在此路线图中进行并最终实现全部约束条件.试验结果显示,该方法可以实时获得实现TF/TA2的三维航迹.     

高保真语音数字信号获取系统设计与实现

给出了高保真数字信号获取系统的结构,分析了为生成高保真语音数字信号文件应注意的器件选择、电路设计和编程实现方法,总结了高保真数字信号获取系统四个主要环节,提出了相应的设计原则。     

一种基于DDS的战术信息栅格信息分发方法

战术信息栅格信息分发是实现战术级环境下信息按需共享的核心技术。遵循发布/订阅模型,提出一种基于数据分发服务(DDS)的战术信息栅格信息分发方法,给出了实现框架和应用实例,并进行了性能实验。实验结果表明,该方法具有较好的信息分发处理性能,基本满足战术信息栅格信息分发应用的需求。     

时钟漂移对GPS/BD2组合系统精度影响分析

首先针对GPS时钟漂移,推导了计算位置误差的表达式,然后对GPS/BD2组合系统的时钟漂移进行了分析和修正,并利用模拟信号源提供的信号进行了仿真.结果表明:经过时钟漂移修正后,定位精度有了一定的提高,验证了仿真结果.     

高速/超高速碰撞效应研究

高速/超高速碰撞会产生大量破片,并伴随闪光、等离子体等现象.高速碰撞材料受冲击产生射流及破片高温会引起碰撞闪光现象,获得了碰撞等离子体电磁场强度的变化规律.采用数值仿真与理论分析相结合的方法,获得了高速碰撞破片云团分布规律.     

爆炸成型弹丸侵彻靶板的数值仿真

基于LS-DYNA的动力学分析通用有限元程序,对爆炸成型弹丸形成和侵彻靶板过程进行了数值仿真。建立了数值仿真模型,利用数值模拟技术实现了弹丸的形成以及不同药型罩结构对爆炸成型弹丸形成的影响,实现了侵彻过程中弹丸的变形与靶板的破坏状况可视化,同时对仿真结果进行了分析。通过对爆炸成型弹丸侵彻靶板的数值仿真,为开展爆炸成型弹丸毁伤机理研究奠定了良好的基础。     

Effects of total pressures and equivalence ratios on kerosene/air rotating detonation engines using a paralleling CE/SE method

In this paper, the kerosene/air rotating detonation engines(RDE) are numerically investigated, and the emphasis is laid on the effects of total pressures and equivalence ratios on the operation characteristics of RDE including the initiation, instabilities, and propulsive performance. A hybrid MPI + OpenMP parallel computing model is applied and it is proved to be able to obtain a more effective parallel performance on high performance computing(HPC) systems. A series of cases with the total pressure of 1 MPa, 1.5 MPa, 2 MPa, and the equivalence ratio of 0.9, 1, 1.4 are simulated. On one hand, the total pressure shows a significant impact on the instabilities of rotating detonation waves. The instability phenomenon is observed in cases with low total pressure (1 MPa) and weakened with the increase of the total pressure. The total pressure has a small impact on the detonation wave velocity and the specific impulse. On the other hand, the equivalence ratio shows a negligible influence on the instabilities, while it affects the ignition process and accounts for the detonation velocity deficit. It is more difficult to initiate rotating detonation waves directly in the lean fuel operation condition. Little difference was observed in the thrust with different equivalence ratios of 0.9, 1, and 1.4. The highest specific impulse was obtained in the lean fuel cases, which is around 2700 s. The findings could provide insights into the understanding of the operation characteristics of kerosene/air RDE.     

Thermodynamics and performance of Al/CuO nanothermite with different storage time

The storage stability of energetic materials is important for its application. Here, the storage stability of Al/CuO nanothermite, which was prepared by electrospray method and stored with different storage time, was systematically researched. The activation energy of Al/CuO nanothermite was calculated by differential scanning calorimetry (DSC). The ignition temperature and the curve pressure history of Al/CuO nanothermite was measured using ignition temperature measuring device and constant-volume pressurization tests, respectively. Further, the thermites were characterized by X-ray Diffractometer (XRD), X-ray photoelectron spectroscopy (XPS), scanning electron microscope (SEM) and Transmission electron microscopy (TEM). The results show that the morphology of the thermites did not change significantly. The activation energy was decreased from 254.1 kJ/mol to 181.8 kJ/mol after storage for 13 months. When stored for 0, 7 and 13 months, the peak pressures of Al/CuO nanothermite were 685.8 kPa, 626.3 kPa and 625.5 kPa, respectively. In addition to the ignition temperature, it was 775 ℃, 739 ℃ and 754 ℃, respectively. This result indicated that the ignition and combustion properties of Al/CuO nano-thermite are obviously reduced when stored for a long time, at room temperature.     

沉浸式虚拟维修仿真中的穿越处理问题研究

沉浸式虚拟维修环境下,物体间发生穿越的碰撞问题可以分为3类:1点接触,2点接触和3点及3点以上接触。采用改变碰撞物体的运动方向和距离的方式来避免物体间穿越现象的发生。并以实例的方式对其有效性进行了验证。     

弹道冲击下层合板破坏模式及抗弹性能实验研究

以舰用轻型复合装甲研究为背景,针对不同纤维增强种类(包括玻纤织物 C400、C200、SW220 和芳纶纤维织物T750)以及不同面密度层合板结构,在6.2 g刚性微曲面柱形弹弹道冲击下的防护能力展开实验研究,着重讨论了层合板结构弹道冲击下破坏模式、弹体初始侵彻速度及面密度与抗弹能力和抗弹效率之间的关系,认为不同的破坏模式体现了不同的吸能特性和纤维失效机理.