baground-subtraction-methods

介绍了蒙特卡罗(Monte Carlo) 方法,即随机模拟方法,提出了任意分布随机数的产生原理 及方法,并用算例说明蒙特卡罗方法的使用过程,同时用χ2 拟和优度法验证了其合理性. 关键(Montcarlo simulation)

说明：  介绍了利用Matrix VB插件实现从VB中调用MATLAB函数的具体方法，利用该方法，可大大提高 VB程序的计算和绘图能力，增强用户开发人机界面友好的计算程序的能力(Introduced the use of Matrix VB plug-in implementation to call MATLAB functions from VB specific method, this method can greatly improve the VB procedure of calculation and graphics to enhance the user friendly interface developed the capacity calculation program)

MUSIC Code in Matlab

使用单连接聚类的方法，对两类问题进行分类(Clustering method using a single connection, two kinds of classification problems)

多尺度LBP的原代码，用于人脸识别，在orl数据库中的识别率达97 以上。(Multi- scale LBP original code, used in face recognition and the recognition rate of over 97 in orl database.)

digital control systems in Z on Matlab

To design a Band Stop Filter using Blackman window matlab code with example

说明：  主要是Peter Zillmann, Wolfgang Rave, and Gerhard Fettweis编写的turbo码在ofdm中信道均衡的文章。(Mainly Peter Zillmann, Wolfgang Rave, and Gerhard Fettweis prepared turbo codes for channel equalization in ofdm article.)

这里我们针对三级固体火箭进行研究，主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差（相差 ）时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中，火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行，第二、三级飞行时已在大气层外，此时可忽略气动力的影响。(Here we study for three solid rocket, the main consideration at every level when the engine thrust and state arising the moment the rocket off point perturbation deviation (difference) in the presence of specific impulse and engine test bias. Outside of the rocket flight dynamics equations can be established on the ground coordinate system launch, the rocket s first stage, the second and third stages according to a fixed elevation angle of flight procedures, and the second, when the third flight already in the atmosphere, this when can ignore the effects of gas dynamics.)

单载波频域均衡系统matlab仿真程序。信道使用的是多径瑞利衰落信道。(The single-carrier frequency domain equalization system Matlab simulation program. Channel using multipath Rayleigh fading channels.)