用matlab的实现调制解调方式

左右相机的16对棋盘格标定图像，缺少测试数据的可以下载

一个BOT的四维模型，内有容积卡尔曼滤波算法(CKF)和本人所提的嵌入式容积卡尔曼滤波(ECKF)算法的比较

基于MATLAB通过对未编码，汉明码 ，循环码及卷积码的信噪比进行比较，比较它们之间的性能

几个交通仿真的Matlab程序，主要是交通流等仿真，有关智能交通方面

这个里面有两本：一本PDF。不必仔细看，了解即可，它主要讲关于安装的细节。一本chm：《Ubuntu 实用学习教程》。这个要非常仔细地看，我就是从这个chm开始的。看完了这个chm教程后，建议大家再去下载这个教程，也是菜鸟级别的书，不过讲得要深入一些：从Windows转向Linux教程。我没具体看这本的教程，我直接借的图书馆的书，是随便找的——很老的一本书（好书都被其它同学给借走了），是清华大学出版的。我不是非常推荐这本书，我感觉即不太适合菜鸟看，也适合菜鸟看，因为里面对shell讲得比较细，当你有了一些linux操作经验后shell是必须得学的，此时你看此书才觉得深入浅出。因为此书

matlab小波去噪详解超全超全有程序,小波去噪，硬阈值软阈值

SigmaPlot中文教程——SigmaPlotSampleGraphs实例作图

zencart评论csv批量导入插件,1.39,1.5版本均支持。

基于ISO标准利用刃边法求解图像MTF曲线

计算飞机气动特性的软件的说明书，主要应用于概念设计和初步设计阶段TABLE 2AERODYNAMIC OUTPUT AS A FUNCTION OF /CONFIGURATION AND SPEED REGIME● OUTPUT A∨A| LABLED OUTPUT ONLY FOR CON FIGURATIONS WITH STRAIGHT TAPERED SURFACESA OUTPUT ONLY WITH EXPERIMENTAL DATA INPUCONFIGURATION SPEEDSTATIC AERODYN AMIC CHARACTERISTIC OUTPUTDY NAMIC STABILITY CUTPUREGIMECLSUBSONICBODYTRANSONICSUPERSONICHY PERSONICWINGTRANS0NC口▲|口「口百口SUPERSONIC●{a!口口日口HYPERSONIC口!口D口口HORIZONTALTRANS0NCa|▲▲口口|口白SUPERSONIC·a|口口口·『●|●IY PERSONICVERTICAL TAILSUBSONICOR VENTRALTRANSONIC口FINA sUPERSONIC.「百|口HY PERSONICSUBSONICWING-BODYRANSONC口口口o口SUPERSONIC●d|口HY PERSON百口HORIZONTALTRANS0NIc口口口TAIL- BOOYSUPERSONIC口口0口HY PERSONICSUBSONICVERTICAL TAILTRANSONIC口VENTRAL FIN-2 SUPERSONIC.BODY●●|●|●HYPERSONIC口w|NG-B0D￥△ SUBSONIC■口|口|口|口|a口|aaa0|口aaaaTRANSONICO|口TAILSUPERS0NC口百|百口「口。|口HYPERS0NC口口|口口口口口口SUBSON1C●VERTICAL TAILTRANS0NC▲口VENTRAL FINA SUPERSONIC●●|●●HYPERSONICING BOOYSUBSONICHORIZONTAL口日|a口口a「aa}aTRANSONIC|▲|▲▲▲口A SUPERSONIC O。|。口}口|口口|口VERTICAL TAILVENTRAL FINHYPERS0NC口口c1 THE EFFECTS OF JET POW2PELLER POWER, AND GROUND PROXIMITY MAY BE OBTAINED FOR THESE CONFIGURATIONS IF THE REQUIREDNAMELISTS ARE INPUT, THE EFFECTS OF POWER AND GROUND EFFECTS ARE INCLUDED ONLY IN THE SU!C LONGI TUDIN AL STABILITY RESULTS2 DY NAMIC STABILITY RESULTS ARE THE SAME AS WING-BODY3 TKIN VERTICAL TAIL RESULTS MAY BE OBTAINED FOR THESE CONFIGURATIONS IF THE REQUIRED NAMELIST IS INPUTTHESE EFFECTS ARE INCLUDED ONLY IN THE SUBSONIC LATERAL STABILITY DATAREFER TO DATCOM HANDBOOK FOR METHOD LIMITATIONS IF OUTPUT IS NOT OBTAINED5 AVAILABLE ONLY IN COMBINAT:ON WITH A WING OR TAILCC