xianxing

卷积码的编码与维特比译码的相关仿真，比较它们的性能(Convolutional codes of coding and Viterbi decoding of the relevant simulation to compare their performance)

说明：  自适应算法网格设定，紧接着上一篇上载内容(getmesh，putmesh)

说明：  matlab的认知无线电仿真代码,主要是能量检测的仿真。(matlab CR)

link hfss and matlab (vbscript)

RTL8100 circuit application

说明：  物流选址matlab代码，简单易懂，有注释。(Logistics choose matlab code, easy to understand.)

802.11同步算法的matlab仿真与FPGA实现，非常适合工程应用(802.11 synchronization algorithm matlab simulation and FPGA realize, very suitable for engineering applications)

说明：  很好的matlab的bpsk仿真源代码程序,是由很有经验的工程师编写(good Matlab BPSK simulation source code procedures, is very experienced engineers prepared)

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)

系统辨识与自适应控制源程序 各章节源程序代码(System recognition and adaptive control )