duochiduxiaobodebianyuanjiancesuanfa

最优化方法 HookeJeeve 和Powell算法 matlab 程序 简单例子(Optimization method and the Powell algorithm matlab program HookeJeeve simple example)

线性拟合程序,航天器运算结果可以进行拟合运算(Linear fitting procedure, spacecraft operations to fit the computing results can be)

The file introduces a modelling for the photovoltaic array panel.

PCA算法，用于用于主分量分析，挺好用的！！！！！！！！！(PCA algorithm for principal component analysis used, very good use! ! ! ! ! ! ! ! !)

Alamoudi in Matlab,this is the advance matlab version.

invers fuzzy logic control for induction motor

matlab小波算法实现，有源程序,可以实现多种图像处理过程(matlab wavelet algorithm, has the source code, you can realize a variety of image processing)

3D FDTD程序中加入平面波传播。确保它从一侧传出，通过空间，且在另一侧消失。(3 D FDTD program to join plane wave propagation. Ensure that it spread from one side, through the space, and on the other side disappear.)

Language Implementation Patterns - Terence Parr. How to design your own programming language.

精密控制结构需要满足先进飞机的使命和对其引航的要求。这就要求飞行器的性能必须满足在低空飞行，低速飞行和大迎角攻击性飞行，全天候，昼夜工作的条件，并且新的控制技术应该成熟。这项工作提出了飞行控制时，状态变量和控制输入是由预先确定的限制范围内的系统控制系统的设计理念。在设计过程使用动态规划的概念。其基本思想涉及非二次泛函最小化。由于一系列限制因素，建议使用光滑函数。同时提出了该综合方法的优点。我们利用对F-18战斗机的纵向控制配置来说明该设计方法。(Indirect adaptive control for reconfigurable flight control is advocated. Specifically, online static system identification using a moving window/batch estimation is implemented. The ensuing linear regression is augmented with an intercept. The intercept parameter is included to address the effects of trim change associated with the occurrence of a control surface failure. Parameter estimate information is used to adjust the inner loop’s control gains, and a command derived from the intercept estimate is fed forward to automatically retrim the aircraft. The tracking performance of this automatic retrimming method, which relies on system identification, surpasses the conventional approach of exclusively relying on integral action for retrimming. These adaptive and reconfigurable flight control concepts are illustrated in the context of a fighter aircraft’s pitch plane dynamics. The novel adaptive and reconfigurable flight control system successfully handles a 50 per cent horiz)