1分下载 矩阵论 程云鹏 第三版教材加答案

【实例简介】使用matlab GUI编写。具有实时采集心音信号（计算机声卡输入），或者直接读入现存的心音音频信号（wav格式）。快速傅里叶变换，DB6，小波滤波，香农熵分析后给出分析结果，可给出心率，有无心音分裂，第一二心音时间间隔是否正常等。是个测试程序，功能比较少。

计算radon-wigner变换的Matlab程序

用Java写成的小游戏，一共有六个，都蛮有趣的包括打字游戏2个，简单的乒乓球游戏2个，小人对打游戏，雪花移动游戏

经典的稀疏表示SRC算法，适合广大人脸识别的同学使用参考-The classic sparse representation SRC algorithm

这是用马尔克夫模型进行数据预测预测的数据是数学建模中 流感疫苗的爆发情况

采用kalman滤波算法，对含噪声的语音信号进行降噪，能够取得较好的效果。

屏幕自适应程序，使用时直接调用即可。里面包含测试程序，可执行文件等。

包含最全的，ansys中所可能用于分析的材料属性和特征。

本程序时利用verilog硬件描述语言开发FPGA。设计使用按键作为输入控制，在VGA显示器上实现贪吃蛇游戏，包含控制VGA显示器显示图片。

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