Lyapunov-MRAC

最小二乘支持向量机,用于多元非线性回归分析,非线性拟合与预测(Least squares support vector machine for multi-linear regression analysis, nonlinear fitting and prediction)

Matlab编写的弹道分析算法-MATLAB源代码(Trajectory analysis algorithms written in Matlab-MATLAB source code)

高阶谱分析工具箱（HOSA）中choices函数。(HOSA tool box s demo will call a function name choices. Copy this file to one of your MATLEB search path to fix the choices problem. )

系统辨识与MATLAB仿真程序与剖析夹.iso《系统辨识及其MATLAB仿真》附带的光盘(System identification and analysis with MATLAB simulation program folder. Iso " System Identification and MATLAB" supplied CD-ROM)

十折交叉验证算法的代码，我用的比较简单，希望大家能够喜欢(Ten-fold cross-validation algorithm code, I use relatively simple, hope that we can love)

Asynchronous machine simulation over matlab using schematic blocs and parameters comparison

single phase SPWM modulation with filter

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.)

Radar Systems Analysis and Design using MATLAB 英文第三版，2013年最新版，压缩包中含有全书的pdf与书中所有代码(Radar Systems Analysis and Design using MATLAB English, Third Edition, 2013, the latest version, pdf compression and book package contains all of the code book)

ELM 极限学习机的核函数 MATLAB程序，用于深入研究和改进极限学习机(Kernel MATLAB program ELM Extreme Learning Machine for further research and improvement Extreme Learning Machine)