基于粒子群算法和遗传算法的PID参数优化

介绍怎么通过matlab完成线性代数的运算,入门教程，简单易懂！(How to introduce, through the completion of linear algebra matlab computing, Getting Started tutorials, easy-to-read!)

万勇革著的MATLAB与信号处理，非常好的一本书，许多程序十分结合工程实践(WAN Yong-ge with the MATLAB and signal processing, a very good book, many programs are combined engineering practice)

说明：  直流电机双闭环控制simulink仿真模型(DC motor control simulink simulation model of double loop)

用MALLAT算法对信号分解,并给出各分解信号的频谱(with MALLAT right signal decomposition algorithm, and gives the signal decomposition of the spectrum)

The most widely used transform for image fusion at multi scale is Wavelet Transform since it minimizes structural distortions. But, wavelet transform suffers lack of shift invariance & poor directionality. These disadvantages are overcome by using our proposed method that is Un-decimated Discrete Wavelet Transform.

说明：  有关自动控制方面的惯性环节响应，matlab仿真程序(control of the inertial response link, Matlab simulation program)

MATLAB Simulations for Radar Systems DesignMATLAB_Codecirc_array.rar(MATLAB Simulations for Radar Systems Design MATLAB_Code circ_array.rar)

matlab中移动字符对象，有源程序 并附有说明 直接复制到matlab的m文件中即可运行(matlab moving characters in the object, there is a direct copy the source code with a note to the matlab m-file to run)

用matlab读入各个通道载荷数据，计算最大幅值应力，并保存。没有次数。(max load )

说明：  螺旋桨PID控制 In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate. (PID control of the propeller In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate.)