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jouying_V4.6

于 2016-12-26 发布文件大小:8KB

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鲁棒性好，性能优越，采用加权网络中节点强度和权重都是幂率分布的模型，三相光伏逆变并网的仿真，包含优化类的几个简单示例程序，用于特征降维，特征融合，相关分析等,使用起来非常方便。 ( Robustness, superior performance, Using weighted model nodes in the network strength and weight are power law distribution, Three-phase photovoltaic inverter and network simulation, Optimization class contains several simple sample programs, For feature reduction, feature fusion, correlation analysis, Very convenient to use. )

文件列表：

jouying_V4.6.m,13846,2016-05-04

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Build_Noiselets
这是一个Noiselet变换的程序，应该会比较有用，有兴趣的可以到MGA网站查看其具体应用。(This is a Noiselet transformation process, should be more useful, interested can go to the MGA Web site to view their specific applications.)

2010-05-31 12:03:57下载

积分：1
ea-turbo-v2
turbo codes in matlab

2013-12-20 00:41:52下载

积分：1
matlabh
some exercices with matlab

2013-12-23 18:33:13下载

积分：1
reverberation_shum
Settles an invoice time of reverberation. A test signal - white noise. The analysis to be made through 1/3 octava filters. Time of record of a signal of white noise 1 second. Duration of the analysis of process of reverberation 1 second. Time of transients which arise during reverberation is considered.

2010-10-21 20:07:47下载

积分：1
DFP
optimation method DFP

2012-04-09 22:55:46下载

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KalmanAll
kalman 滤波器，初学者的参考,最好先学习一下其推到过程(kalman filter kalman filterkalman filterkalman filterkalman filterkalman filter)

2011-11-24 16:24:24下载

积分：1
Newton_Steffensen
本源程序是基于Newton迭代改进的Steffensen加速法，具有更好的收敛性质(The source code is based on the Newton iteration acceleration method to improve the Steffensen, has better convergence properties )

2011-12-02 15:25:18下载

积分：1
puma3dfiles
The modeling and attitude stabilization control problems of a four-rotor vertical takeoff and landing unmanned air vehicle (UAV) known as the quadrotor are investigated.The quadrotor’s attitude is represented by the unit quaternion rather than Euler angles to avoid singularity problem. Taking dynamical behavior of motors into consideration and ignoring aerodynamic effect, a nonlinear controller is developed to stabilize the attitude.The control design is accomplished by using backstepping control technique.The proposed control law is based on the compensation for the Coriolis and gyroscope torques. Applying Lyapunov stability analysis proves that the closed-loop attitude system is asymptotic stable. Moreover, the controller can guarantee that all the states of the system are uniformly ultimately bounded in the presence of external disturbance torque.The effectiveness of the proposed control approach is analytically authenticated and also validated via simulation study.

2014-09-04 19:00:04下载

积分：1
process-control-sub
Simulate PID for process control using matlab

2013-09-22 11:01:20下载

积分：1
PS2
power spectrum density for different digital communications schemes

2013-09-20 09:30:42下载

积分：1

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jouying_V4.6

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