Modicon-Quantum-Safety-PLC-Reference-Manual

利用偏移量插值实现图像的透视变换（运用了双线性变换原理）(Offset interpolation using the image perspective transformation (using the bilinear transformation principle))

It is great model of one part of engine diesel model. This particular file contains model of intake manifold.

MIMO script for BER computation BPSK

哈哈镜各种变形原代码，读入待制作的图片，实现图片的缩小放大、水平外凹、水平外凸、梯形变形、三角形，S形和波浪型。(DistortionLi various deformation original code to be read into the production of pictures, the pictures achieve narrow enlarge level Au, Spirogyrate level, trapezoidal deformation, triangle, and the S-wave type.)

异步双馈风力发电感应电机的网侧变换器，电压外环电流内环控制，可以运行(The grid side converter of double fed wind power asynchronous induction motor, voltage loop and current loop control, you can run)

Matlab中用GUI设计一简单计算器。(err)

一个估计garch（1,1）的matlab程序(matlab code for estimating garch（1,1）)

利用matlab编写的界面程序，实现控制系统的设计与分析(Prepared using matlab interface program of the control system design and analysis)

qam 16 reseiver diversity matlab file

这里我们针对三级固体火箭进行研究，主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差（相差 ）时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中，火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行，第二、三级飞行时已在大气层外，此时可忽略气动力的影响。(Here we study for three solid rocket, the main consideration at every level when the engine thrust and state arising the moment the rocket off point perturbation deviation (difference) in the presence of specific impulse and engine test bias. Outside of the rocket flight dynamics equations can be established on the ground coordinate system launch, the rocket s first stage, the second and third stages according to a fixed elevation angle of flight procedures, and the second, when the third flight already in the atmosphere, this when can ignore the effects of gas dynamics.)