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csminit
Fixed 7/17/93 to use inverse-hessian instead of hessian itself in bfgs
- 2010-03-04 16:58:33下载
- 积分：1
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slidingmode
滑模变结构控制MATLAB仿真 经典书籍 刘金琨(a book of sliding mode Liu Jinkun)
- 2009-06-05 23:36:40下载
- 积分：1
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DS_SS
DIRECT SEQUENCE SPREAD SPECTRUM
- 2015-03-07 22:35:35下载
- 积分：1
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MTALABandsimulink
用四阶龙格库塔法求非线性系统的输入相应，同时用simulink建模比较。
(Using fourth-order Runge-Kutta method for the corresponding input nonlinear systems, and modeling using simulink comparison.)
- 2009-03-28 14:20:09下载
- 积分：1
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16QAM
这个是本人编写的构建16QAM的源代码，详细阐述了里面construction 调整解调。这是个完整的程序并且可以运行(I am writing this is to build the source code for 16QAM, which details the construction adjustment demodulation. This is a complete program and can run)
- 2011-07-03 23:47:31下载
- 积分：1
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AES
code for AES to to encrypt data
- 2013-02-02 19:09:22下载
- 积分：1
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softmax
说明： MNIST手势识别数据库进行softmax回归分类，直接运行softmaxExercise.m文件即可运行。(The MNIST gesture recognition database is classified by soft Max regression and can be run directly by running the softmaxExercise. m file.)
- 2019-05-18 15:31:21下载
- 积分：1
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emgmm
EM算法估计GMM的matlab版本的源代码，适合给类机器学习问题(EM algorithm estimates GMM Matlab version of the source code, suitable for the type of machine learning problems)
- 2006-06-23 16:35:01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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fam
Cyclostaionary spectrum estimation by FAM method
- 2012-05-25 22:55:24下载
- 积分：1
