PID

关于神经网络非线性系统的辨识，模糊控制器等程序。(With regard to neural network, nonlinear system identification, fuzzy controller and other procedures.)

说明：  oqpsk,qpsk信号的调制与解调并绘制出调制后的图形。(oqpsk, qpsk signal modulation and demodulation, and draw graphics modulated.)

多种频谱校正算法，不同加窗情况下的幅值校正及matlab程序。(Variety of spectrum correction algorithm, the amplitude correction and matlab program in different windows circumstances.)

固有时间尺度分解算法，实现对时间序列信号的多尺度分解，提取多分量信号中的单分量成分。(Intrinsic time scale decomposition algorithm to achieve multi-scale decomposition of the time series signal to extract a single multi-component signal component ingredients.)

广义雅克比算法，求解小维数矩阵全部特征值的变换类算法(failed to translate)

12脉二极管整流MATLAB仿真12脉二极管整流MATLAB仿真(12-pulse diode rectifier 12-pulse diode rectifier MATLAB simulation MATLAB simulation)

说明：  matlab R2012a 超级学习手册随书源代码(Matlab R2012a Super Learning Manual with Book Source Code)

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)

False nearest neighbors

InSAR里面的goldstein相位解缠绕的MATLAB源代码，绝对能够运行(InSAR which the goldstein flow phase unwrapping method for MATLAB source code is absolutely able to run.)