source_code_vn0dzg

Matlab中的MFDFA工具箱，非线性时序分析，预测，H指数，维度。(Muti-fractal Detrended Fluctuation Analysis (MFDFA) Toolbox in Matlab)

use alamouti for communication system.

ESPRIT DOA算法的稀疏表示求解，程序中使用了凸优化工具箱(ESPRIT DOA algorithm of sparse representation, the program used in the convex optimization toolbox)

Neural Network - MLP Network - matlab source.

单载波频域均衡中，信道是一个很关键的问题，信道估计的好坏也直接影响系统的性能，确定一个好的信道估计序列是至关重要的，chu 序列是一种很好的估计序列(Single-carrier frequency domain equalization, the channel is a very critical issue, good or bad channel estimation is also directly affect the performance of the system to determine a good channel estimation sequence is critical, chu sequence is a good estimate of the sequence)

matlab ctrllab30, CtrlLAB is a group of MATLAB functions which provide graphical interface to perform feedback system analysis and design tasks.(matlab ctrllab30, CtrlLAB is a group of MATLAB functions which provide graphicalinterface to perform feedback system analysis and design tasks.)

MITAB Library mitab-0.1

此源代码,是一个非常适合研究与学习用的电力系统仿真软件源码，是一种基于mattlab的，有非常好的界面、仿真库等等，能进行PF、CPF、OPF等一些计算。 (This source code is a very suitable for research and study used in power system simulation software source code is a matlab-based, and has very nice interface, the simulation database and so on, can P )

在某初教机的线性模型基础上，建立了飞机的纵向和横向传递函数，分析了模型参数的不确定性，通过使用MATLAB中的NCD模块对飞行控制系统及PID控制器等参数进行优化，设计出了飞机的自动驾驶仪高度保持和航向保持模式。这种方法既避免了复杂的计算和编程，又使系统具有较好的稳定，陛、动态性能和鲁棒性，克服了飞机模型参数随着高度和速度的变化（即模型参数存在不确定性）而需要按照多个不同高度和速度的飞行区域设计一系列控制器的缺点(early in a plane of the linear model, based on the aircraft's vertical and horizontal transfer function, Analysis of the model parameters of uncertainty, MATLAB through the use of the NCD Blocks flight control system and PID controller parameters for optimization, design of the aircraft's automatic pilot systems, and maintain a high degree course-keeping mode. This method not only avoids the complex calculation and programming, the system has good stability, Her Majesty, dynamic performance and robustness. overcome the aircraft model parameters with the height and speed of change (that model parameters uncertainty exists) and the need to not more than with the height and speed of regional flight controller design a series of shortcomings)

goldmin method - use a root in polynomial or function / iterative method