GUI

基于的FSK的matlab，完整的程序，有能相关的说明和注释，有需要的朋友下载吧~(Based on the matlab FSK, complete program and relevant instruction and comments, the need to download friends ~)

此文件汇集了为各种数字滤波器消噪，应用广泛(This file is a collection of denoising widely used for a variety of digital filters )

数值分析，Matlab的一个方程的迭代解法，很有用的(Numerical analysis, iterative solution of an equation of Matlab, very useful)

说明：  可以修改文字的颜色、大小、字体。还可以对文字的方格和粗细进行设定。(You can modify the text color, size, font. The text can also be configured grid and thickness.)

matlab中的绘图命令介绍，有助于初学者了解基本的绘图知识(drawing commands in the matlab help beginners understand the basic knowledge of drawing)

智能微电网粒子群优化算法,微源：光伏、风机、发电机、储能等(Smart Microgrid PSO, micro sources: photovoltaic, wind turbines, generators, energy storage, etc.)

MPPT最大功率点跟踪控制，搭建了并网历程，并且使用MPPT控制。(MPPT maximum power point tracking control, build the grid-connected process, and use MPPT control.)

Bpsk代码，用Matlab 产生BPSK代码(Bpsk code, BPSK code generated by Matlab)

说明：  关于无线传感器的LEACH改进的协议，是基于改进粒子群算法的，很有帮助(LEACH for Wireless Sensor improved protocol is based on improved particle swarm algorithm, useful)

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)