基于LSSVM的缺失飞行数据组合填补方法

针对飞行数据的特点,将基于最小二乘支持向量机的一元填补方法和多元填补方法相互结合,提出了一种缺失飞行数据的组合填补方法。该方法将两者优势互补,既能反映出变量自身的变化趋势,同时也利用了相关变量间的作用信息,增强了算法的可靠性,提高了数据填补的精度。实验结果表明了所提方法在缺失飞行数据填补中的有效性和适用性。     

消防部队基层指挥员作战指挥能力评估研究

通过建立消防部队基层指挥员作战指挥能力评估模型,采用模糊综合评判和层次分析法(AHP),对基层指挥员作战指挥能力给出了较为精确的计量,可以了解掌握基层指挥员自身实力和存在不足,也为上级用人提供依据.     

雷达目标识别的频域极小极大法

本文研究了雷达目标识别过程中关于目标的编码、分类特征的提取与选择等问题。提出了利用极小极大原则从频域中获取目标特征系数的方法,论述了它的数学框架以及寻求最佳解的算法步骤。利用实测的目标散射数据进行试验研究,结果表明了本文理论的正确性及其方法的有效性。     

网络集群现象的特点及对策研究

网络集群现象是指在互联网络环境中,由某一舆论引发,多数人参与,发生观点的群体性激化,从而对现实社会产生一定的冲击和影响的事件。针对网络集群现象的特点,着重从参与主体、交互方式、传播方式、情绪表现、影响因素、处理难度等方面进行研究,并提出防范对策。     

基于Nastran优化的某导弹结构模型修正

为了对某型号导弹结构建立合理的有限元全弹模型,基于Nastran的灵敏度分析及优化功能,首先对初始导弹模型设计参数进行了灵敏度分析,并确定优化设计的设计变量,然后以模态试验结果为优化目标,对其进行动力学优化,得到修正模型.结果表明,修正后模型的计算结果与试验结果偏差有很大程度的改进,符合了工程的使用需要.     

航空自导深弹攻潜模型与仿真

针对反潜巡逻机使用磁探仪和自导深弹的攻潜效能研究,提出了一种基于蒙特卡洛法的计算模型。在建立攻潜坐标系的基础上,给出了连投深弹射击深度的定义;结合磁探仪定位原理,提出了基于峰值追踪的定位目标和连投攻击的方法。仿真结果表明,该方法能够提高命中概率。给出了目标分布和连投深弹的散布模型,根据攻潜过程和命中判定条件,进行了攻潜效能的计算,并仿真分析了影响攻潜效能的主要因素,研究了投弹间隔的确定方法。     

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.     

A reusable planar triggered spark-gap switch batched-fabricated with PCB technology for medium-and low-voltage pulse power systems

Triggered spark-gap switch is a popular discharge switch for pulse power systems. Previous studies have focused on planarizing this switch using thin film techniques in order to meet the requirements of compact size in the systems. Such switches are one-shot due to electrodes being too thin to sufficiently resist spark-erosion. Additionally, these switches did not employ any structures in securing internal gas composition, resulting in inconsistent performance under harsh atmospheres. In this work, a novel planar triggered spark-gap switch (PTS) with a hermetically sealed cavity was batched-prepared with printed circuit board (PCB) technology, to achieve reusability with low cost. The proposed PTS was inspected by micro-computed tomography to ensure PCB techniques meet the requirements of machining precision. The results from electrical experiments demonstrated that PCB PTS were consistent and reusable with lifespan over 20 times. The calculated switch voltage and circuit current were consistent with those derived from real-world measurements. Finally, PCB PTS was used to introduce hexanitrostilbene (HNS) pellets in a pulse power system to verify its performance.     

Effect of metal powders on explosion of fuel-air explosives with delayed secondary igniters

In order to improve the energy level of fuel air explosive(FAE) with delayed secondary igniters, high energetic metal powders were added to liquid fuels mainly composed of ether and isopropyl nitrate. Metal powders' explosive properties and reaction mechanisms in FAE were studied by high-speed video, pressure test system, and infrared thermal imager. The results show that compared with pure liquid fuels, the shock wave overpressure, maximum surface fireball temperature and high temperature duration of the mixture were significantly increased after adding high energetic metal powder. The overpressure values of the liquid-solid mixture at all measuring points were higher than that of the pure liquid fuels. And the maximum temperature of the fireball was up to 1700 ℃, which was higher than that of the pure liquid fuels. After replacing 30％of aluminum powder with boron or magnesium hydride, the shock wave pressure of the mixture was further increased. The high heat of combustion of boron and the hydrogen released by magnesium hydride could effectively increase the blast effect of the mixture. The improvement of the explosion performance of boron was better than magnesium hydride. It shows that adding high energetic metal powder to liquid fuels can effectively improve the explosion performance of FAE.     

Numerical and experimental study on the response characteristics of warhead in the fast cook-off process

The response characteristics of the warhead under thermal stimuli conditions are important to the safety improvement. The goal of this study is to obtain data on the warhead in the fast cook-off process. In this paper, a numerical calculation method is proposed, whose reliability is supported by comparison with experimental results. Through the numerical calculation, the temperature distribution, temperature change, and ignition time are acquired. The numerical results show that the ignition time is 76 s after the warhead started to burn and that the maximum temperature of the explosive's outer surface is 238.3 C at the ignition time. The fast cook-off experiment of the warhead is implemented so as to get the flame temperature and reaction grades that are not available through numerical calculation. The experimental results show that the overpressure fails to reach the preset minimum value which is equivalent to 6 kg of TNT and that the reaction grade is deflagration. The research results have reference value for the design of the warhead and the reduction of detonation risks.