卫星遥测数据实时压缩算法设计与实现

为了满足多星并行遥测数据处理和海量数据高并发分析的性能需求,便于后续进行数据挖掘、智能预警,本文提出并实现了一种卫星遥测数据实时压缩算法。针对遥测数据的特点,提出了遥测自适应分类方法,采用改进型RLE（Run Length Encoding,行程编码）压缩和增量压缩结合的算法,结合数据库技术,实现了遥测数据的压缩。在某型号卫星研制项目中,采用了该算法进行数据压缩,统计分析表明：该算法起到了很好的压缩效果。     

针刺C/C复合材料高温力学性能

文摘采用材料超高温力学性能设备及高温应变测试系统,对针刺C/C复合材料拉伸、压缩性能进行了研究。结果表明:针刺C/C复合材料具有明显的拉、压双模量特性,拉、压模量均随着温度的升高而线性下降,且拉伸模量下降更快;针刺C/C复合材料拉伸、压缩强度均随温度升高而先升高后降低,1 600℃时拉伸强度达到最大值,1 200℃时压缩强度达到最大值;其拉伸破坏为脆性断裂,断口呈现45°豁口;其压缩破坏为典型剪应力引起的压缩失效,破坏面倾角为40°~50°。     

Progressive damage behaviors of woven composite laminates subjected to LVI,TAI and CAI

This paper seeks to deal with progressive damage behaviors of woven composite laminates subjected to low-velocity impact(LVI), tension-after-impact(TAI) and compression-afterimpact(CAI). The LVI, TAI and CAI tests were conducted on woven carbon fibre lamina3238 A/CF3052 and woven glass fibre lamina 3238 A/EW250 F, and the time-dependent LVI contact force and deflection curves, static TAI and CAI load versus displacement curves were determined and discussed. A modified progressive damage model wa...     

Energy absorption features of 3-D braided rectangular composite under different strain rates compressive loading

There are huge potential applications of 3-D braided composite in aerospace engineering because of the non-delamination feature of the composite under impact loading. This paper presents the analysis of energy absorption features of 3-D braided composite under compression with different strain rates. The 3-D 4-step rectangular braided composite coupons were tested on a material tester MTS 810.23 and a split Hopkinson pressure bar (SHPB) apparatus to obtain out-of-plane and in-plane compression stress vs. strain curves at quasi-static and high strain rate state. The failure modes and energy absorption features of the 3-D braided composite under different strain rates were analyzed both in time domain and frequency domain. The energy absorbed by the 3-D braided composite increases with the strain rate. From fast Fourier transform (FFT) analysis of compression stress vs. time histories, the power of energy absorption of the 3-D braided composite increases with strain rate and mostly concentrate on the high frequency region. While for quasi-static compression, the power distributes in very narrow frequency region and also is less than that in high strain rates. This feature corresponds to the different damage and energy absorption mechanisms of the 3-D braided composite under quasi-static and high strain rate compression.     

Application of dynamic recrystallization model in AZ12 magnesium alloy rolling process

To deeply understand the dynamic recrystallization behavior of as-cast AZ12 magnesium alloy in deformation process, the uniaxial hot compression experiments were implemented through systematic isothermal compression experiments. The true strain of thermal compression experiments was set to 50% with temperatures of 200, 250, 300, 350, 400 °C and the strain rates of 0.001, 0.01, 0.1, 1 s^?1. The Dynamic Recrystallization (DRX) kinetic model of AZ12 magnesium alloy was established and the accuracy of this model was verified. The model is used to predict the volume fraction of the sheet obtained by rolling through different rolling passes under the condition of consistent total reduction (50%). And the predicted results are in good agreement with the experimental results.     

面向星载应用的空间域四叉树层次化图像压缩算法

为满足卫星应用领域对高分辨率遥感图像实时传输与存储的要求，针对该类图像特征，提出基于空间域四叉树数据结构的图像数据亚采样与多模式自适应预测编码相结合的压缩算法。该算法使用四叉树数据结构与三种预测编码模式，针对图像块纹理差别，自适应地选取相应的亚采样与量化编码方式，通过采样方式与量化方式的变化，达到保存高分辨率遥感图像细节与小目标绝不丢失的要求，实现了对遥感图像中目标边缘和变化剧烈的细节的高保真效果，同JPEG相比，恢复图像峰值信噪更高、图像纹理细节保持能力更强。利用具有可编程序门阵列器件物理实现上述算法，获得高速图像压缩专用芯片，该芯片数据处理速度达到288Mbit／s，功耗低于1W。     

脉冲燃烧风洞点式油流技术在压缩拐角流动显示中的应用

为在脉冲燃烧风洞上应用油流技术,针对该类设备马赫数6条件下气流总温高(可达1650K)、有效试验时间短(约300ms)、小动压条件下显示油"流不动"等困难,提供了一种技术解决方案。试验设备为中国空气动力研究与发展中心Φ=600mm脉冲燃烧风洞。采用两个多级压缩楔模拟高超进气道外压缩面,其中三级压缩楔偏转角为6°,7°和8°,两级压缩楔偏转角均为10°。运用高速摄像方法获得了点式图谱的动态变化过程。三级压缩楔8°拐角上游油点在200ms内流过了拐角,并向下游移动了足够长度,可判断该拐角处气流不产生分离。两级压缩楔油流结果则显示风洞尾气会显著改变图谱分布。     

基于小波变换的静止图象压缩系统

本文实现了一个基于小波变换的静止图象压缩系统。包括以下工作：用引入了小波包思想的小波变换将图象分解到一个完备的多分辨的空间上去，对系数做标量量化，利用小波变换的方向性进行扫描和游程编码，之后对低频部分作ＡＤＰＣＭ编码，最后，系统的输出是嵌入式的。实验结果表明，对于静止图象的压缩，本文的结果在一定程度上好于ＪＰＥＧ     

进口总压径向畸变对扩压叶栅弯叶片流场性能的影响

为进一步探讨低速条件下弯叶片在扩压叶栅中的适用条件，用数值分析的方法研究了五种径向总压畸变的进口条件对扩压叶栅中弯叶片作用的影响。结果表明：进口总压畸变的型式能够影响弯叶片在扩压叶栅中的作用，影响分别为畸变层厚度的影响和主流区总压与端壁总压之差的影响。在一定的范围内畸变层越厚或压差越大，弯叶片对吸力面角区低通流区的密流增加越明显，从而更大程度地改善了端区的通流能力和流场性能，也极大地降低了叶栅损失。     

含分层损伤复合材料层板压缩分层疲劳扩展研究

采用基于Mindlin一阶剪切理论的连续壳单元,建立了预测含分层损伤复合材料层板在压缩疲劳载荷作用下的分层扩展3D模型,分析了含穿透分层复合材料层板在压缩疲劳载荷作用下的分层扩展行为。利用累积损伤理论,对层板内出现的各种典型损伤进行相应的刚度折减,并在循环加载过程中对材料性能进行强度弱化。利用虚裂纹闭合技术(VCCT)计算分层前缘处的能量释放率,结合混合断裂判据判断分层是否扩展,进而得到压缩疲劳载荷作用下分层扩展规律。计算模型通过大型商用有限元软件和自编程序实现。通过对数值仿真结果和试验结果进行比较,验证了模型的合理性和准确性。