Desktop

此文件是基于ARToolKit的开发包上的再次开发，上面显示一个一个立方体，并加以稳定的程序，对增强现实有很好的指教。(This document is based on the development of ARToolKit developed again on the package, shown above, one by one cube, and the procedures to be stable, for augmented reality have a good advice.)

dv-hop算法的matlab仿真编码 (dv-hop algorithm matlab simulation code)

算是一个小小的教程，交给初学者如何使用matlab，进行聚类分析，里边包含源码及示例。(Is a small tutorial to the beginners how to use Matlab, cluster analysis, and the inside contains the source code and examples.)

This is consist of converting the matlab code to dll using C++ code

Adaptive filter theory book by simon haykin s matlab codes

最炫民族风的matlab程序源代码，在matlab论坛找到的，供大家娱乐(The most unusual national wind Matlab source code in matlab Forum found for all entertainment)

基于matlab的FFT算法运用；64点和128点的FFT的幅度谱(64-point and 128-point FFT amplitude spectrum use matlab FFT algorithm )

kriging插值算法。虽然用得较少，但是很实用。(kriging interpolation algorithm. Although less used, but very practical.)

Matlab/Simulink 滑膜控制(sliding mode control)

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)