esvga

SOMVIS软件学习材料，高纬网络及其可视化(SOMVIS software, learning materials, networks and visualization of high-latitude)

function g=distance_classify(A,b) 距离判别法程序。 输入已分类样本A（元胞数组），输入待分类样本b 输出待分类样本b的类别g 注：一般还应计算回代误差yita 输入已知分类样本的总类别数n 每类作为元胞数组的一列(function g = distance_classify (A, b) from the Criterion procedures. Input samples have been classified A (cell array), the importation of samples for classification b output samples for classification g categories b Note: the calculation should also be back on behalf of the general error input yita of the total known types of classification of the number of samples n each Cellular-type array as a)

应用matlab计算心理声学参数loudness的工具。(loudness calculation)

making admitance matrix

遗传算法的具体实现 打开直接运行 可以出结果 本程序主程序为第一个函数 注释很详细 修改隶属度函数可以求出你要求的函数的值 (The concrete realization of the genetic algorithm to open run directly on the results of this program the main program for the annotation of the first function in great detail to modify the membership function can be calculated the value of the function you have requested)

buck pid仿真 BUCK 的 PID 控制，调整参数，更深入理解 PID 控制 学习使用 MATLAB ，并在 MATLAB 中建立电力电子仿真电路模型(buck pid)

A code for pseudo coloring the images

GA2 for single Machin Problem

说明：  该程序试图考察一组数据服从哪种分布（正态，指数或双边指数），并利用K-S检验对各种分布作了检验。(The program attempts to examine a set of data subject to which distribution (normal, exponential or bilateral index), and use KS test has been tested in a variety of distributions.)

说明：  螺旋桨PID控制 In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate. (PID control of the propeller In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate.)