Data-driven prediction of plate velocities and plate deformation of explosive reactive armor

Explosive reactive armor (ERA) is currently being actively developed as a protective system for mobile devices against ballistic threats such as kinetic energy penetrators and shaped-charge jets. Considering mobility, the aim is to design a protection system with a minimal amount of required mass. The efficiency of an ERA is sensitive to the impact position and the timing of the detonation. Therefore, different designs have to be tested for several impact scenarios to identify the best design. Since analytical models are not predicting the behavior of the ERA accurately enough and experiments, as well as numerical simulations, are too time-consuming, a data-driven model to estimate the displacements and deformation of plates of an ERA system is proposed here. The ground truth for the artificial neural network (ANN) is numerical simulation results that are validated with experiments. The ANN approximates the plate positions for different materials, plate sizes, and detonation point positions with sufficient accuracy in real-time. In a future investigation, the results from the model can be used to estimate the interaction of the ERA with a given threat. Then, a measure for the effectiveness of an ERA can be calculated. Finally, an optimal ERA can be designed and analyzed for any possible impact scenario in negligible time.     

自由漂浮空间机器人关节故障锁定位置辨识

针对自由漂浮空间机器人在关节故障情况下关节锁定位置的辨识问题,根据其线动量守恒和角动量守恒特性,建立了关节故障锁定位置辨识的误差模型,提出了利用混沌粒子群优化(CPSO)搜索关节故障位置的辨识算法。最后采用虚拟样机技术,建立了空间机器人系统的虚拟样机,对空间机器人系统进行动力学仿真,获取了运动数据,采用此数据对提出的关节故障位置辨识算法进行了有效性验证。     

H/HCLZ-Ⅱ型测量组合导航系统总体设计

介绍了Ｈ／ＨＣＬＺ－ Ⅱ型测量组合导航系统的功能、组成及软硬件设计．近４年的实船使用表明,该系统功能强、使用方便、可靠性好,研制是非常成功的．     

基于SRUKF仅测角导航的空间交会闭环控制协方差分析

针对基于仅测角导航的空间交会问题,开展了采用线性协方差进行闭环控制误差快速分析方法的研究。建立了基于SRUKF (Square Root Unscented Kalman Filter) 的仅测角导航算法并推导了观测敏感矩阵,构建了基于多脉冲Hill制导的闭环控制线性协方差分析模型。经算例验证,本文提出的闭环控制协方差分析结果与Monte Carlo打靶结果能够很好吻合;该方法适用于采用传统Extended Kalman Filter (EKF)的仅测角导航问题,但其迹向位置的估计存一个与该方向控制误差方差相当的偏心,其误差椭圆的长轴和短轴分别比基于SRUKF的估计结果大了24.68%和20.56%。此外,由于采用了QR分解和Cholesky 因子更新两种高效的代数运算,基于SRUKF的协方差分析模型要比基于EKF的协方差分析模型在计算速度上快了10%。     

Numerical investigation on cooling performance of filter in a pyrotechnic gas generator

As a key part of the pyrotechnic gas generator,the filter not only removes the particulate matter but also cools the hot gas to a safe level.This paper aims to improve the understanding of the basic heat and flow phenomenon in the gas generator.The pyrotechnic gas generator is modelling by a simplified filter structure with fiber arrays.A finite-volume model of the heat and fluid flow is proposed to simulate the detailed multi-dimensional flow and energy conversion behaviors.Several verification results are in good agreement with data in different references.Simulation results demonstrate that the filter can not only absorb heat from the gas but also cause the high intensity enhancement of the heat transfer.The per-formance difference between inline and staggered arrays is also discussed.The findings of the study put a further prediction tool for the understanding and design of the filter system with fibers.     

杂波环境下红外传感器滤波算法

基于定向概率数据关联滤波(DPDAF)算法,根据红外传感器对目标方位角与俯仰角分辨率不同的特性修正了似然函数,并利用等效观测噪声协方差阵修正滤波增益的思想,构造了一种旨在提高红外传感器跟踪性能的修正定向概率数据关联滤波算法.蒙特卡洛仿真结果表明,新算法对红外目标的跟踪具有比DPDAF更好的跟踪性能.     

侧壁激波诱导下凹腔燃烧室冷态流场实验观测

在单凹腔燃烧室中引入侧壁激波,为研究燃烧室内部流动特性,采用纳米粒子平面激光散射技术和粒子图像测速技术对全尺寸玻璃燃烧室模型进行流场观测,获得了冷态流场展向和法向的瞬态灰度图及平均速度场。实验结果表明:在远壁面区域,凹腔内部速度与密度都较低;引入侧壁激波后,近壁面区域凹腔与主流的质量与动量交换增强,速度与密度升高;受到侧壁激波影响,燃烧室底壁边界层不再均匀,凹腔中后部产生大规模低速区,具有明显三维特性。     

三轴磁强计轨道确定

未来卫星的发展趋向于微小型化 ,采用小型化、廉价和中等精度的自主导航系统是非常必要的。利用三轴磁强计量测得地磁场矢量在仪表坐标系中的分量 ,并通过卡尔曼滤波器来确定卫星的轨道参数。仿真算例结果表明 ,三轴磁强计定轨方案具有一定的精度 ,能满足卫星定轨精度的要求。     

机动目标跟踪的非线性算法

卡尔曼滤波器对线性高斯滤波问题能提供最优解, 而对目标运动模型、观测方程等要求的非线性就不再适合,提出了一种机动目标自适应非线性粒子滤波算法-" 粒子滤波器"(Particle Filters PF)法, 这种方法不受线性化误差和高斯噪声假定的限制,适用于任何状态转换或测量模型, 分析比较了粒子滤波(PF)与扩展卡尔曼滤波算法(EKF) 的滤波精度、运算量等方面指标.给出了基于典型非线性模型的算法仿真, 仿真结果表明粒子滤波新方法优于EKF对机动目标跟踪.     

基于粒子群优化算法的低空突防航迹规划

本文提出了运用粒子群优化算法来对飞机低空突防进行航迹规划的方法。首先,说明了飞机突防需要满足的物理限制和战术要求。其次,根据低空突防航迹规划约束多,计算复杂的特点引入粒子群优化算法,并且对其进行简要的介绍。应用粒子群优化算法对低空突防战术进行航迹规划。最后实验结果表明,该方法能够对飞机低空突防过程规划出可行的飞行航迹。