SysIdentifyHomework

模式识别中贝页斯分类器的MATLAB实现，且用不同颜色标记了分类点和错分点(pattern recognition Pui page Andean classification of MATLAB and use different color marker of separation points and the wrong points)

FFT变换,获得采样数据基本信息，时域图，频域图,FFT transform, sampling data basic information, time domain, frequency chart(FFT transform, sampling data basic information, time domain, frequency chart)

波束形成MUSIC，信号在波数域进行MUSIS算法(Beamforming MUSIC, the signal in the wavenumber domain MUSIS algorithm)

对在MATLAB编程环境下的模糊推理过程进行确定性分析，分析了模糊推理的过程和参数选择方法，并进行了方针证明。(MATLAB programming environment in the fuzzy reasoning process of uncertainty analysis, analysis of the fuzzy reasoning process and parameter selection method, and carried out policies to prove.)

运用matlab7.0编写的应用sa处理旅行商问题(The preparation of the application of the use of matlab7.0 Traveling Salesman Problem sa deal)

用拉丁超立方采样方法模拟具有相关性的数组代码(Latin Hypercube Sampling Method cubic correlated array simulation code)

显示hello的matlab源代码 几句matlab的代码(Hello, matlab source code shows a few matlab code)

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)

simulink ac too dc simpower in matlab

量子计算与量子优化算法的部分程序，感兴趣的可以下载学习~~(Quantum computing and quantum optimization algorithm part of the program interested you can download to learn ~ ~)