LQR

这是一种模拟退火的MATLAB的代码有用请下载(if it help,please go ahead)

采用行均值相减法抑制温度场的非线性影响，增强目标点，利用形态学方法抑制背景并保留高亮区，搜索局部极大值，利用阈值分离出目标，实现红外点目标的检测(enhancement of point target are carried out by inhibiting nonlinear influence in temperature field with line average subtracting，Inhibiting background and maintaining high brightness area are implemented by using Top-Hat operator morphological filtering，then The targets are separated off from searching for local maximum。this program realize the detection the infrared small target)

Matlab Package for Estimation of distribution algorithm

for fast optimize programming in matlab

非常详细的介绍RS编码的小书，内附有MATlab程序。(The little book of a very detailed description of RS coding, enclosing a MATlab program.)

梁在横向荷载作用下的挠度曲线和应力分布，matlab实现的有限元程序，单元为8结点等参元 将matlab工作目录设为解压后的文件夹 依次执行 main postprocessing 两条命令(matlab program for FEA)

该程序是通过MATLAB平台作出的修正型平面二次包络蜗杆的仿真图.(The program is made through the MATLAB platform modified Planar Double-Enveloping Worm Simulation Fig.)

雷达系统仿真类的，天线波束中，产生一个线性阵列信号。(Radar simulation system and the like, the antenna beam, the signal to generate a linear array.)

esay to use but long program if want to play around with

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.)