nelder

由Patton开发的由MATLAB实现的COPULA源代码(By Patton developed by MATLAB source code to achieve COPULA)

modifi bf load flow in matlab

通信系统的Matlab代码，包括括通信原理书中的大多代码可直接使用。 (Matlab code of the communication system, including most of the code including communication theory book can be used directly.)

一个关于线程池的小demo，windows环境下，可以直接运行。( A little on the thread pool demo, windows environment, can be directly run.)

Integrating m-files functions and algorithms in C++ applications

这个是自己实现的matlab与c++的一个接口。 是用c++语言实现的(This is the realization of our own Matlab and c of an interface. Is the C Language)

BakeCode通信原理的巴克码模拟编码实现(BakeCode communication principle of Barker code simulation Coding)

vb调用matlab——多项式拟合 vb调用matlab——多项式拟合(vb call matlab- polynomial fitting vb call matlab- polynomial fitting)

利用matlab进行滑动平均法消除趋势项(Using matlab trend term moving average method to eliminate)

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.)