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jieguo3
matlab 模式识别识别数据,循环处理(Matlab pattern recognition to identify data processing cycle)
- 2012-06-27 16:29:14下载
- 积分:1
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adaptiveAR
AR自适应滤波器,用Kalman滤波器跟踪AR模型的吸收变化(adaptive AR model,use kalman filter to trace the variance of ar coeffience)
- 2013-09-09 10:18:13下载
- 积分:1
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MATLAB
MATLAB科学计算与可视化仿真-源代码(MATLAB)
- 2010-05-08 21:47:36下载
- 积分:1
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ofdm_ber
Program for ofdm and its BER performance
- 2010-05-12 16:55:15下载
- 积分:1
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Nonparametric-Genetic-Clustering
Nonparametric Genetic Clustering
- 2014-02-20 10:16:32下载
- 积分:1
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Matlabtongji
武汉大学遥感信息工程学院MATLAB期末的大作业,对遥感影像进行处理并且进行统计求方差平均数,并绘制图像(Great job of Remote Sensing Information Engineering, Wuhan University MATLAB end of remote sensing image processing and statistical variance of the average demand and draw the image)
- 2014-02-18 19:08:21下载
- 积分:1
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LMS_RLS_MVDR_SMI
自适应波束形成算法,有需要的可以下载看看(Adaptive beamforming algorithm, there is a need can be downloaded)
- 2013-07-13 16:27:15下载
- 积分:1
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Mycold
在matlab软件中,自己编程实现的一个分类算法,算法首先采用kmeans与fcm聚类分析方法进行采样,然后利用svm对选取得样本进行分类(In matlab software, own programming to achieve a classification algorithm, the algorithm first used fcm kmeans cluster analysis methods and sampling, and then use the elections to obtain samples for svm classification)
- 2013-12-24 19:29:47下载
- 积分:1
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compare
compare with 2 image
- 2010-12-26 01:08:54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