k-means-matlab

信号分析处理：信号时宽与带宽。此例程为高斯信号及其频谱的分析(Signal analysis and processing: signal width and bandwidth. This routine for the analysis of the Gaussian signal and its spectrum)

对一个给定的状态转移矩阵求其联合分布矩阵，联合熵，平均互信息量以及共熵。可以画出平均互信息量的曲线(For a given state transition matrix of their joint distribution matrix, the joint entropy, mutual information and the average total entropy. Can draw the curve of the average mutual information)

说明：  visual c++ 开发的MemFile的源代码， 喜欢的可以下(visual c MemFile development of the source code, like they can)

《MATLAB R2008图形与动画编程实例教程》的源代码--第一章(" MATLAB R2008 examples of graphics and animation programming tutorial" source code- the first chapter)

说明：  模糊聚类matlab，是一个等价关系模糊聚类的程序！(fuz)

绘制一条与控制多边形相切的三次均匀b样条曲线。(A degree-3 uniform b spline curve, it is tangent to its control polygon.)

matlab中的siso设计工具，讲的比较细致！(siso design tools in matlab speak carefully!)

Il existe par ailleurs de nombreuses commandes permettant de contrô ler les palettes de couleurs utilisées pour la représentation graphique, en particulier la commande colormap

用于盲源信号分离,可以将源信号通过混合矩阵进行混合，通过求解分离矩阵，实现源信号的分离。(Using ICA algorithm to solve blind source separation problems,this procedure can separate the source commendably.)

说明：  月球软着陆仿真：在停泊轨道上，探测器在脉冲制动的作用下，经霍曼变轨，下降到距月面大约 15 公里的近月点，该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段，由于探测器的初始速度很大(1.692km/s)，所以主制动段制导律设计的主要目的就是高效抵消此速度，将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)