1

说明：  无线通信系统仿真英文版，实用性很强，是一本不可多得的好书(Principles of Communication System Simulation with Wireless Aplications)

compressive sensing ALGORITHIM CODE FOR MATLAB

this file implement stochastic method in pattern recognition

the is cuK converter designed in matlab by me.. it is closed loop operated one.. which cam regulated line as well as load

AP-FFT频谱校正方法,需要自己改进一部分。(AP-FFT spectrum correction method, need to improve their own part.)

图像截图完成一个简单的多媒体应用程序，包含：多媒体信息的获取、处理、展现三个基本过程。(this is a snapshot code)

The lecture program c

CDMA 语音编码，在MATLAB环境下可直接运行(CDMA speech coding)

说明：  图像处理（验证码识别）程序 内含事例(Image processing (validation code identification) program contains examples of)

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)