层次分析法在修理级别分析中的应用

修理级别的非经济性分析有多个结果时,很难确定产品的合理修理级别,若采用经济性分析,数据采集难,并且可操作性差.因此,提出用层次分析法来决断产品合理修理级别的方法,以提高修理级别分析方法的可操作性,并为其工程化提供一种思路.     

反解法在再入机动弹道设计中的应用研究

简要分析了一般的再入机动弹道设计方法,即正解法.针对正解法对模型依赖性强和对初值非常敏感的问题,提出了一种基于误差补偿的机动弹道设计方法——反解法.该方法从弹道终端出发反解弹道,将计算结果误差转化为机动点参数误差,再通过关机点或中制导的调整进行误差补偿,从而有利于命中精度和打击效果的实现.仿真结果表明,该方法计算简便,对工程应用有一定的参考价值.     

武汉长江隧道疏散方式选择与观测分析

阐述了隧道疏散的各种方式,说明了武汉长江隧道采用下沉式滑道的纵向疏散方式的原因,对武汉长江隧道疏散系统进行了详细演习测试,并对当前拥挤状态下的通车条件进行了分析,认为只要保持交通通畅,加强管理,隧道下沉式纵向疏散系统可以满足通行客车时的人员疏散安全。     

有限群的极大子群的正规指数

有限群的结构与其子群性质间的关系问题是群论的一个重要研究方向,通过群的极大子群、正规子群、半正规子群、极大子群的正规指数等去研究群的可解性,超可解性、幂零性等,已有一系列结果.应用极小反例方法,利用有限群极大子群的正规指数,得到了一个有限群是π-可解群的充分条件,2个有限群是π-可解群的充分必要条件.     

基于GeoHash索引的A算法优化

A*(A Star)算法进行最短路径计算时,一般采用曼哈顿函数作为最优邻接点的评估标准,在算法执行的过程中,需要对每一步每个邻接点进行计算,判断出当前最优邻接点,然后迭代执行下一步,在数据量较大的情况下,算法的时间复杂度呈几何增长.使用GeoHash索引算法代替曼哈顿函数作为评估标准,在有地理坐标信息的网络拓扑中进行最短路径查找,直接以GeoHash编码索引值作为判断标准,进行快速查找.GeoHash值是经纬度经过一系列编码转换后的实际值,能够拓扑网格中的属性值,减少算法的计算时间,优化算法的时间复杂度.提高A*算法在道路规划、运行调度、无人驾驶路径分析时的最短路径计算时间,可增加实际应用广泛性.     

基于双谱切片小波包的雷达体制识别技术

根据机械扫描雷达、一维相控阵雷达和二维相控阵雷达扫描方式的差异,通过对3种体制雷达进行双谱分析、切片化处理以及小波包分解,提出了双谱切片小波包的概念,并根据此特征用支持向量机对不同体制的雷达进行识别.仿真结果表明:该方法在噪声占比为0～20％时,可分性好,并且在噪声占比增大时,通过该特征仍能对不同体制的雷达进行有效识别.     

欧盟太空安全政策与发展动向

欧盟具有相对成熟的太空技术,处于国际太空力量发展的第一梯队,其太空安全政策是在基于维护太空自主权的前提下,寻求太空与安全防务政策的统一,从而实现共同外交和安全政策的整体目标,目前已取得了较大进展。本文认为,从未来发展来看,面对有限的太空资源优势和脆弱的太空环境,欧盟将会继续利用其技术优势和集体力量,努力保障其太空关键基础设施安全和太空自主权,同时进一步将太空安全重点向军事竞争领域聚焦,将其作为拓展战场空间维度的重要途径。     

交通场景行人穿越检测方法进展研究

随着自动驾驶和计算机视觉技术的飞速发展,人们对交通安全的重视程度越来越高。其中,交通场景中行人穿越检测问题是研究的热点与难点之一。对行人穿越检测这一领域进行了综合评述,并对未来研究进行了展望。按照行人试图穿越、正在穿越及穿越预测三个阶段进行分析,首先分析了基于行人姿态穿越意图的研究进展(试图穿越),包括人体姿态、数据驱动和高斯动力学模型三个方面;其次讨论了基于轨迹跟踪的穿越行为检测方法(正在穿越);然后概括了基于轨迹预测的行人穿越检测方法(穿越预测);最后总结了现阶段比较新颖的多传感融合、车路协同、车联网等研究角度,并对未来该领域需重点发展的方向提出建议。     

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.     

Transverse relaxation characteristic and stress relaxation model considering molecular chains of HTPB coating based on pre-strained thermal aging

In order to accurately describe the transverse relaxation characteristic and stress relaxation modulus of HTPB coating during pre-strain thermal aging process, a one month thermal aging test was carried out at 70 C with pre-strain of 0％, 3％, 6％ and 9％, respectively. The low-field 1H NMR and stress relaxation modulus tests were carried out for HTPB coating at different aging stages. The stress relaxation model considering the molecular chains was proposed according to the changes of crosslinking chain and dangling chain of HTPB coating during pre-strain aging. The results showed that with the increase of aging time, the decay rate of transverse relaxation curve became faster, the transverse relaxation time decreased, the value of combined parameter qMrl increased, the proportion of crosslinking chain decreased, while the proportion of dangling chain increased. Moreover, the stress relaxation modulus increased, the crosslinking network structure of HTPB coating became denser and the degree of cross-linking increased. At the initial aging stage, the pre-strain will destroy the crosslinking network structure of HTPB coating to a certain extent. With the increase of aging time, the effect of pre-strain will gradually weaken and the influence of aging on materials will gradually increase. The correlations between the stress relaxation model considering the molecular chains and the test results were more than 0.9950, which can accurately describe the stress relaxation modulus of HTPB coating during the pre-strain thermal aging process.