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KNN
KNN是常用的一个对于大维数据分类的方法，大家可以参考下(KNN classify)
- 2014-09-20 18:26:57下载
- 积分：1
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kmeans
Matlab 写的kmeans slc 算法
还包括实验报告，其中有实验结果图的对比(Matlab kmeans and slc algrithms,
reports with experimental results attached
I hope it is useful for you )
- 2010-06-29 21:53:13下载
- 积分：1
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highstepup-circuit
This simulation by MATLAB s simulink for boost converter circuit "HIGH STEP-UP CONVERTER"
- 2011-05-27 01:03:58下载
- 积分：1
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2D_feature_finding
粒子追踪测速的相关程序，所使用的算法为最邻近原则，通过粒子链表形成匹配(Particle tracking velocimetry procedures, the algorithm used for the nearest neighbor principle formed by particles linked list match)
- 2012-11-30 22:32:31下载
- 积分：1
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process
peak filter design for audio signal
- 2010-11-22 04:45:43下载
- 积分：1
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xgohan
the model incon telecharge for interne
- 2010-05-15 07:03:39下载
- 积分：1
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processMotion1.m
processMotion1.m MATLAB处理地震波的程序(processMotion1.m MATLAB processing seismic program)
- 2014-11-25 19:57:27下载
- 积分：1
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基于PCA的SVM分类
说明： 选择“BreastCancer”数据集，使用支持向量机(SVM)对其进行分类。作为对比，第一次对特征集直接进行支持向量机分类，第二次对特征集进行主成分分析法的特征提取后，再对特征提取后的特征集进行支持向量机分类。并且对比和分析了两次分类的结果。(The BreastCancer data set is selected and classified by Support Vector Machine (SVM). For comparison, the first time the feature set is classified directly by support vector machine, the second time the feature set is extracted by principal component analysis, and then the feature set is classified by support vector machine. The results of the two classifications are compared and analyzed.)
- 2020-06-20 10:20:02下载
- 积分：1
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time9
关于时钟一个基本的Matlab动画程序，可以使初学者了解动画程序的应用。(On a basic clock Matlab animation program that allows beginners to understand the application of animation process.)
- 2009-01-01 13:10:28下载
- 积分：1
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Reconfigurable-flight-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)
- 2011-05-02 12:39:11下载
- 积分：1
