BA

说明：  该文件包含用MATLAB实现的OFDM 的源程序(Channel estimation for a MIMO-OFDM system)

雷达系统仿真用matlab (RADAR SYETEM )

HHT(hilbert haung transform)

在ofdm系统中空时格状码编译码方式，与ofdm结合性能的比较(in OFDM systems hollow when trellis coding- decoding methods, combined with OFDM Performance Comparison)

字典学习及稀疏编码 非常好的工具箱!!!!!!!!(dictionary learning and sparse coding perfect toolbox!!!!!!!!!!!!)

利用matlab实现的数字波束形成算法，适合初学者学习。(Implementation of Digital Beamforming Algorithms)

实现FM的调制解调 实现FM的调制解调 实现FM的调制解调(matlab FM matlab FM matlab FM)

simulink model of the basic function of soft drink machine

机器学习算法， 使用Fisher score进行特征选择。(Machine learning algorithms, feature selection using Fisher score.)

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)