LMS

对螺旋桨进行初步的设计和分析,在matlab环境下，通过GUI界面设置输入参数可得到初步的设计结果(Preliminary propeller design and analysis, in the matlab environment, set the input parameters available through the GUI interface preliminary design results)

This paper deals with software LABREG for identification and control of real processes. The LABREG operates in MATLAB environment using toolboxes SIMULINK, Ident, Control and Real Time.

2010年WCCI会议发表的二型模糊系统EIA降型方法(Presented in 2010 World Congress on Computational Intelligence, as the latest type reduction algorithm of type-2 fuzzy logic systems. EIA)

这是一个用matlab做的功率谱估计，采用几种方法仿真并比较(This is a matlab to do with the power spectrum estimation, using several methods and compare simulation)

说明：  这是一个关于MATLAB的函数，能够用DEMO打开；使用时首先解压然后转换为M文件即可。很方便的。(It is a MATLAB function, can open the DEMO use first and then converted to M-extracting files. Very convenient.)

Very basic MATLAB code for adaboost

Wind turbine output power vs. rotational speed, with wind speed as parameter

采用滑模控制和RBF网络来控制对象，采用等效滑模控制的方法，即根据系统的确定部分计算出等效控制量，同时利用一个RBF网络对系统的不确定部分进行补偿得到切换控制量。(Using sliding mode control and the RBF network to control the object, using the equivalent sliding mode control method, namely the determination of the system to calculate the equivalent control part of the volume, at the same time using a RBF network of uncertainty on the system parts to be switched to control the amount of compensation .)

unsupervised local discriminative analysis each column is a data

MIT--航空航天工程中的计算方法_概率论方法实例——涡轮叶片中的热传导问题 MIT公开课程--航空航天工程中的计算方法 这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构，空气动力学，动力学和控制，和航空宇宙系统选出的。其技术包括：常微分方程系统的数值积分；偏微分方程式的有限差分,有限体积, 和有限元的离散化；数值线性代数；本征值问题和带有约束的最优化。(MIT- Aerospace engineering calculation methods of probability theory _ instance- turbine blade heat conduction problem in the MIT Open Course- Aerospace engineering calculation methods for this course in aviation and aerospace engineering calculation methods appear of getting started. The application is from aerospace structures, aerodynamics, dynamics and control, and aerospace systems selected. The technologies include: numerical integration of ordinary differential equations systems partial differential equations of finite difference, finite volume, and finite element discretization numerical linear algebra eigenvalue problems with constraints and optimization.)