function wpt

蒙特卡洛模拟 数学建模matlab计算机仿真(Monte Carlo computer simulation of mathematical modeling matlab)

matlab 自己编写的小波去噪算法，没有用到MATLAB自带的函数。(matlab，Written the wavelet denoising algorithm by myself,Don t use MATLAB own letter)

基于OFDM中的LS和DFT信道估计算法(LS and DFT channel estimation algorithms in OFDM)

Single Underwater Image Enhancement with a New Optical Model

This code implements the affects of linear and non linear kernel.

采用K近邻算法预测时间序列的源代码，希望对大家能有所帮助。(Predict time series using kNN.)

说明：  关于MATLAB程序设计基础的一篇文章，挺好的。(On the MATLAB program design based on an article, quite good.)

精密控制结构需要满足先进飞机的使命和对其引航的要求。这就要求飞行器的性能必须满足在低空飞行，低速飞行和大迎角攻击性飞行，全天候，昼夜工作的条件，并且新的控制技术应该成熟。这项工作提出了飞行控制时，状态变量和控制输入是由预先确定的限制范围内的系统控制系统的设计理念。在设计过程使用动态规划的概念。其基本思想涉及非二次泛函最小化。由于一系列限制因素，建议使用光滑函数。同时提出了该综合方法的优点。我们利用对F-18战斗机的纵向控制配置来说明该设计方法。(Indirect adaptive control for reconfigurable flight control is advocated. Specifically, online static system identification using a moving window/batch estimation is implemented. The ensuing linear regression is augmented with an intercept. The intercept parameter is included to address the effects of trim change associated with the occurrence of a control surface failure. Parameter estimate information is used to adjust the inner loop’s control gains, and a command derived from the intercept estimate is fed forward to automatically retrim the aircraft. The tracking performance of this automatic retrimming method, which relies on system identification, surpasses the conventional approach of exclusively relying on integral action for retrimming. These adaptive and reconfigurable flight control concepts are illustrated in the context of a fighter aircraft’s pitch plane dynamics. The novel adaptive and reconfigurable flight control system successfully handles a 50 per cent horiz)

线性系统根轨迹法在matlab环境下的实例与分析应用(Root locus method in linear system matlab environment and analysis of application examples)

this file denoise the pcg signal by wavelet and find the best wavelet who denoise the pcg signal