一种利用CUDA技术实现雷达余辉效果的方法

雷达PPI显示器余辉效果的好坏直接影响雷达模拟器的逼真程度,从而影响受训人员的训练效果。为实现高度逼真的雷达余辉效果,克服余辉模拟中坐标变换及余辉计算对运算速度需求较高的问题,利用新近出现的CUDA并行处理技术将在CPU上处理耗时较多的坐标变换及余辉计算搬移到GPU上来实现,克服了传统雷达余辉模拟方法中存在的不足。同时,传统余辉模拟方法中无法实现的高转速扫描余辉模拟,以及由于目标数据致使天线转速不稳等问题也得以解决,使用该方法可以实现导航等多型雷达的高转速扫描线余辉模拟。利用该方法研制的雷达训练模拟器已装备到某训练基地,用于雷达兵实际的教学、训练和考核,取得了良好的效果。     

建筑中庭排烟性能化设计与分析

采用火灾烟气控制工程计算方法,设定较适合的火灾场景,对某中庭建筑排烟方式进行性能化分析,得出采取自然排烟方式的可行性建议,并确定了排烟设备的选型、数量和控制方式。     

浅析吸引系数法及其应用

本文通过对吸引系数法的分析,澄清了一个各种刊物在表述吸引系数法时的混淆,并提出了一种吸引系数法的改进方法,使之能够运用于野战指挥通信网中话音和数据业务量的建模。     

作战构想风险性评估模型

作战构想是制定作战方案、定下作战决心的依据,在任务规划中起着承上启下的作用,意义重大.针对构想风险难以定量分析的难题,基于作战构想的组成要素、战场情况分析研判数据,从周密性、机动、打击、防护等角度构建了作战构想风险性评估指标体系,并提出了对各个指标进行定量分析的评估模型.最后,采用实例对提出的方法进行了验证,结果表明,该方法可行有效,避免了定性分析中存在的主观性、模糊性等不足,为作战构想评估提供了新的思路和方法.     

基于GEO SAR辐射的星机协同融合探测系统

为提高机载平台对隐身目标的探测能力,提出一种基于地球同步轨道合成孔径雷达(GEO SAR)辐射、多个机载平台接收的多基雷达协同探测系统,该系统具有覆盖范围广、机载射频隐身、生存能力强等优势.分析了星机协同的作战优势,可获取目标RCS空间闪烁增益、双基RCS增益以及融合增益.分析了星机双基协同探测威力与多基融合探测威力,可提高隐身目标探测距离.通过仿真实验验证了分析的有效性.     

Maneuvering target tracking of UAV based on MN-DDPG and transfer learning

Tracking maneuvering target in real time autonomously and accurately in an uncertain environment is one of the challenging missions for unmanned aerial vehicles(UAVs).In this paper,aiming to address the control problem of maneuvering target tracking and obstacle avoidance,an online path planning approach for UAV is developed based on deep reinforcement learning.Through end-to-end learning powered by neural networks,the proposed approach can achieve the perception of the environment and continuous motion output control.This proposed approach includes:(1)A deep deterministic policy gradient(DDPG)-based control framework to provide learning and autonomous decision-making capa-bility for UAVs;(2)An improved method named MN-DDPG for introducing a type of mixed noises to assist UAV with exploring stochastic strategies for online optimal planning;and(3)An algorithm of task-decomposition and pre-training for efficient transfer learning to improve the generalization capability of UAV's control model built based on MN-DDPG.The experimental simulation results have verified that the proposed approach can achieve good self-adaptive adjustment of UAV's flight attitude in the tasks of maneuvering target tracking with a significant improvement in generalization capability and training efficiency of UAV tracking controller in uncertain environments.     

Survivability assessment of spacecraft impacted by orbit debris

To help optimize the spacecraft design and reduce the risk of spacecraft mission failure, a new approach to assess the survivability of spacecraft in orbit is presented here, including the following three steps:1) Sensitivity Analysis of spacecraft. A new sensitivity analysis method, a ray method based on virtual outer wall, is presented here. Using rays to simulate the debris cloud can effectively address the component shadowing issues. 2) Component Vulnerability analysis of spacecraft. A function"Component functional reduction degree — Component physical damage degree"is provided here to clearly describe the component functional reduction. 3) System-level Survivability Assessment of spacecraft. A new method based on expert knowledge reasoning, instead of traditional artificial failure tree method, is presented here to greatly improve the efficiency and accuracy of calculation.     

亚音速轴流风扇静转子相互作用线谱噪声预报

静转子相互作用线谱噪声是亚音速轴流风扇主要噪声源之一,快速预报该噪声对风扇设计初期的叶片选型和参数设计具有重要意义.因此在叶栅响应函数理论的基础上考虑静转子叶片的相互作用,采用叶片经验尾流模型模拟转子尾流,推导得到静转子叶栅相互作用线谱辐射声功率半经验半理论计算公式.通过与NASA已有的试验模型和计算模型结果对比,验证...     

泡沫塑料衬垫的粘弹性有限元分析

介绍了一种用于聚氨酯泡沫塑料衬垫的粘弹性有限元分析程序,利用积分本构关系计算了轴对称衬垫中的应力松弛。从数值结果可见,当衬垫贮存１０００小时以后,装配应力大约松弛了２５％。     

基于不确定性的末制导初始参数优化设计方法

为量化无动力滑翔飞行器末制导初始参数不确定性的综合影响,提升飞行器落点精度,提出基于不确定性的末制导初始参数优化设计方法。面向飞行器末端高动态打击需求,采用落角约束下的滑模变结构导引律进行实时弹道成型,进而考虑末制导初始参数的不确定性。以落点有效毁伤半径概率和落点圆概率偏差为多优化目标,建立基于不确定性的末制导初始参数及制导律参数优化模型。针对这一不确定性优化模型,研究利用高效全局优化和蒙特卡洛方法,给出末制导初始参数及制导律参数的最优设计方案。仿真结果表明:该方法能显著提升落点精度,为方案设计阶段飞行器末制导交接点的选取提供决策支持。