基于神经网络的离散变结构控制系统

系统研究了基于神经网络的离散变结构控制系统设计方法,提出了几种具体设计方案.神经网络的引入可以使滑模(变结构)控制具备学习与自适应能力,使控制信号得以柔化,从而能够减轻或避免困扰常规滑模控制器的抖振现象,改善控制效果.     

两栖装备乘员可靠性影响因素分析

人的可靠性指的是人在规定的时间内、规定的条件下、完成规定任务的能力,它是整个系统可靠性一个重要的组成部分,作为装甲装备而言,乘员可靠性的高低直接影响到整个装备作战系统可靠性.针对两栖装备的使用环境和使用特点,对影响乘员可靠性的因素进行了分析,得出了结论,对于如何提高两栖装备乘员可靠性有一定的指导意义.     

高速数字电路信号完整性设计

随着电子产品日愈复杂,电路板工作频率不断提升,从而导致信号完整性问题。从工程应用角度阐述了高速电路的概念,列举了典型的信号完整性问题,如反射、串扰、电源和地噪声、定时等,提出信号完整性设计中所应遵循的设计方法,如控制走线长度、特征阻抗控制与计算,仿真技术等,并讲解了真实的设计案例,具有工程应用实际参考价值。     

一种以太网系统监控的双独立互联系统

针对现有技术对高可靠性以太网系统进行监控,具有明显的缺陷和不足之处.提出了一种由用户以太网系统和附加的平衡结构外,总线互连系统组成以太网监控的双独立互连系统.在分析了该系统结构和工作原理的基础上,对系统的可靠度和可用度进行分析计算,为系统的实现提供了重要的依据.     

防空多传感器网络的拓扑优化模型

防空多传感器网络是防空网络化作战体系结构的重要组成部分。针对防空多传感器网络的网络结构模型,研究了已知网络中单元节点的位置和数量,如何最优确定网络中继器的位置、数量及其与单元节点的连接关系,即网络拓扑优化设计问题。最后给出了防空多传感器网络拓扑优化设计的数学模型及其求解方法。     

战场环境下C3I系统效能研究

:C3I系统已成为现代化战争必不可少的重要组成部分 ,其效能分析也越来越受到人们的重视。首先对 C3I系统效能的含义做了分析 ,并在一般效能模型的基础上深入讨论了 C3I系统的作战效能 ,对 C3I系统作战效能的含义和计算进行了研究 ,给出了一种新的评价 C3I系统的方法     

干扰条件下防空兵通信装备系统效能分析

为研究干扰条件下防空兵通信装备系统效能,在ADC模型的基础上构建了ADCF系统效能模型,并结合实例对模型进行了仿真分析.仿真结果显示,该模型能较好反映敌方干扰对通信装备系统效能的影响.提出了干扰条件下提高防空兵通信装备系统效能的措施.     

具有时变时间延迟的混沌保密通信同步方法研究

针对固定时间延迟及时变时间延迟系统,提出了同步控制方案,在实现同步后能有效解决传输时延对保密通信的影响.利用线性矩阵不等式方法设计了同步控制器,应用Lyapunov方法分析了同步误差的收敛性,并运用Schur补引理证明了全局渐近稳定点的存在.     

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 method to determine the shell layout scheme for equipment battlefield damage tests under artillery fire

In this paper,a new method for determining the shell layout scheme is proposed,which can make the equipment damage data by the battlefield damage test resemble as close as possible the actual combat data.This method is based on the analysis of the impact point distribution and effective damage area of equipment.In order to obtain the position of the impact points,an impact point distribution model under artillery fire was established.Similarly,in order to obtain the effective damage area of equipment,the concepts of generalized damage area and task-based equipment functional damage probability were demonstrated,and the corresponding calculation model was established.Through case analysis,the shell layout scheme was effectively obtained,verifying the correctness of the proposed method.