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six
利用MATLAB模拟六边形结构光子晶体光纤的三维结构(MATLAB simulation of the use of hexagonal photonic crystal fiber structure of the three-dimensional structure)
- 2009-05-14 13:51:40下载
- 积分：1
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Runge-Kutta-Fehlberg
Runge-Kutta-Fehlberg法 解初值问题常微分程组(Runge-Kutta-Fehlberg method to solve ordinary differential equations initial value problem)
- 2011-08-18 14:49:08下载
- 积分：1
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matlab-baodian
matlab宝典的书籍，对于学习matlab很有帮助(the matlab Collection of books for learning matlab helpful)
- 2012-11-02 22:53:49下载
- 积分：1
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CRFall
Kevin Murphy编写的CRF条件随机场的matlab工具包，可用于图像处理建模等。(Kevin Murphy for the preparation of the CRF with the airport Matlab tool kits Image processing can be used for modeling.)
- 2006-11-22 15:28:16下载
- 积分：1
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BPSK-QPSK
this code explains the bpsk and qpsk program.
in simulink design...
- 2012-05-03 18:28:52下载
- 积分：1
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xiaobobaonengliangfenxi
小波包提取滚动轴承故障能量特征的matlab程序，大家只要把采集的滚动轴承振动信号数据放入程序中即可使用，希望对大家有所帮助。(Bearing Fault wavelet packet energy feature extraction matlab program, we just put a rolling bearing vibration signal collected data into the program to use, we want to help.)
- 2013-08-11 12:45:19下载
- 积分：1
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scanComPorts
读串口信息,在matlab 环境下读出串口内容(read serial)
- 2013-04-03 11:08:45下载
- 积分：1
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GAencoding
说明： 以MATLAB为工具的实现车间调度问题的源码(MATLAB as a tool to achieve shop scheduling problem source)
- 2010-04-16 19:45:16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
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PR
说明： 基于matlab人脸识别系统的开发与研究，关于人脸识别的研究(failed to translate)
- 2011-05-17 07:21:59下载
- 积分：1
