建筑节能初期设计阶段的能耗模拟与分析

针对建筑节能初期设计阶段,采用建筑环境设计软件Ecotect对某节能示范楼外窗遮阳情况进行模拟分析,得到各朝向外窗的遮阳形式以及大小设计范围,为下一阶段包括外遮阳形式,构造尺寸和各朝向房间的窗墙比、外窗材料选择提供了设计参考.     

光电坐标传感器在光幕靶中的应用

针对光电报靶系统的标校问题,以及可见光光幕靶光电接收器检测灵敏度的一致性和与海量数据的高速采集问题,采用大发射角的LED发光管,设计了光电开关电路和高速采样保持电路,实现了基于光电开关和取样电阻网络的光电坐标传感器,提高了系统的检测灵敏度和一致性,降低了系统设计的难度和成本。试验证明：该方法精度较高,具有良好的应用前景。     

无线传感器网络在环境监测中的应用

低成本、低功耗、自组网的无线传感器网络近年来得到快速发展.对近年来无线传感器网络在环境监测中的应用进展进行系统综述,对国内外各研究小组的研究成果进行对比和分析,最后对无线传感器网络的发展进行总结和展望.     

基于DSP的各向异性扩散滤波算法优化实现

基于各向异性扩散的图像滤波算法可以在有效抑制图像噪声的同时较好地保持边缘细节,但复杂的算法很难满足系统实时性要求.采用基于直方图的统计方法来确定图像各向梯度模值数组的中值,有效提高了确定图像梯度阈值算法的效率.针对ADSP-TS201的结构及指令特点对算法进行了优化实现,较好满足了系统实时性的要求.     

柴油机曲柄连杆机构冲击动力学分析

分别利用MSC.DYTRAN和MSC.ADAMS软件建立了某型柴油机包括曲轴系、活塞组、连杆组及飞轮在内的冲击动力学模型,考虑了惯性力、气缸压力和反扭矩的影响,并利用运动副和接触单元对结合部的实际情况进行了模拟.在此基础上.基于德国BV043/73舰艇抗冲击标准对曲柄连杆机构进行了冲击响应分析,着重研究了曲轴和连杆的冲...     

地空反辐射导弹武器系统作战效能影响评估模型

地空反辐射导弹武器系统融入战术防空体系对防空作战效能的影响如何定量评估是作战运用研究的重要问题。采用阶段概率分析法建立了打击空袭方预警机、电子干扰机对防空作战效能和我方航空兵突击作战效能影响评估模型,通过计算可得出定量数据供作战研究参考。实例计算结果表明地空反辐射导弹武器系统将能极大地提高防空导弹体系作战效能,对于获取防对抗中的信息优势将发挥举足轻重的作用,对地面防空由被动防御向攻防兼备转型将其有重大意义。     

航空集群系统空对地作战效能涌现方法研究

航空集群作战系统通过自组织机制与行为调控机制的有机耦合,产生了新的作战能力,具有能力涌现特点.为评估集群系统作战效能,在机群作战效能评估理论的基础上,采用AHP层次分析法构建了无人-有人机协同作战集群效能涌现模型.结果表明,作战环境威胁越高,集群作战能力的涌现效果越明显,且随着等级的不断提高,能力的涌现不断增加,但是增加的幅度逐渐减缓.该方法的应用可为评估航空集群系统的对地攻击作战能力提供定量参考.     

潜艇应急上浮机动不稳定性建模与仿真

为了避免潜艇在应急上浮过程中,由于较快的上浮速度以及较大的负攻角,水动力呈现强非线性,在横向流作用下潜艇可能产生过大的横倾角甚至失稳倾覆.基于艇体水流入射角和方向角定义下的潜艇非线性水动力描述形式及其试验结果,采用一种新形式的大攻角非稳态潜艇操纵运动仿真数学模型,对高压气吹除主压载水舱后潜艇应急上浮过程的运动状态进行预报.采用拉瓦尔喷管理论对高压气吹除主压载水舱的热力学过程进行建模,并将该过程计算得到潜艇所受的复杂激变力作为潜艇操纵运动仿真数学模型的控制输入,计算结果表明:相较于高压气吹除指数模型,采用的拉瓦尔喷管模型能更为真实地反映实艇高压气吹除过程,对潜艇应急上浮机动的运动状态预报更为准确.应急上浮过程中快速造成较大的尾倾角有利于抑制横倾角的增大,且横倾角主要受水舱吹除顺序的影响,受初始深度的影响较小.根据潜艇事故工况下的初始状态制定有效的高压气应急吹除挽回策略,是抑制应急上浮横倾角的主要手段.     

MF-CFI: A fused evaluation index for camouflage patterns based on human visual perception

The evaluation index of camouflage patterns is important in the field of military application. It is the goal that researchers have always pursued to make the computable evaluation indicators more in line with the human visual mechanism. In order to make the evaluation method more computationally intelligent, a Multi-Feature Camouflage Fused Index (MF-CFI) is proposed based on the comparison of grayscale, color and texture features between the target and the background. In order to verify the effectiveness of the proposed index, eye movement experiments are conducted to compare the proposed index with existing indexes including Universal Image Quality Index (UIQI), Camouflage Similarity Index (CSI) and Structural Similarity (SSIM). Twenty-four different simulated targets are designed in a grassland background, 28 observers participate in the experiment and record the eye movement data during the observation process. The results show that the highest Pearson correlation coefficient is observed between MF-CFI and the eye movement data, both in the designed digital camouflage patterns and large-spot camouflage patterns. Since MF-CFI is more in line with the detection law of camouflage targets in human visual perception, the proposed index can be used for the comparison and parameter optimization of camouflage design algorithms.     

Theoretical and numerical simulation study on jet formation and penetration of different liner structures driven by electromagnetic pressure

The use of a shaped liner driven by electromagnetic force is a new means of forming jets. To study the mechanism of jet formation driven by electromagnetic force, we considered the current skin effect and the characteristics of electromagnetic loading and established a coupling model of"Electric—Magnetic—Force"and the theoretical model of jet formation under electromagnetic force. The jet formation and penetration of conical and trumpet liners have been calculated. Then, a numerical simulation of liner collapse under electromagnetic force, jet generation, and the stretching motion were performed using an ANSYS multiphysics processor. The calculated jet velocity, jet shape, and depth of penetration were consistent with the experimental results, with a relative error of less than 10％. In addition, we calculated the jet formation of different curvature trumpet liners driven by the same loading condition and ob-tained the influence rule of the curvature of the liner on jet formation. Results show that the theoretical model and the ANSYS multiphysics numerical method can effectively calculate the jet formation of liners driven by electromagnetic force, and in a certain range, the greater the curvature of the liner is, the greater the jet velocity is.