ofdmproj_win

经典书籍《通信系统仿真原理与无线应用》chap8部分课后题仿真源代码，用MATLAB编写的(Classic book, )

快速的关闭MATLAB figure窗口，快速的关闭MATLAB figure窗口，(MATLAB figure window closing fast, fast closing MATLAB figure window,)

Matlab/Simulink下的风力发电仿真程序，可用于研究风电并网下稳态、暂态以及故障运行时的系统状态，内附与程序相对应的论文。(Matlab/Simulink simulation program under wind power can be used to study wind power under steady state, transient and fault runtime system state, containing papers that corresponds with the program.)

基于MATLAB受激布里渊散射耦合方程求解，泵浦光向后差分，斯托克斯光向前差分。(Based on MATLAB stimulated Brillouin scattering coupled equations, differential pumping light backwards, Stokes forward difference.)

matlab与vc6.0实现混合编程的源代码，可以实现C++调用matlab数学方法，而无需安装matlab，可以实现快速数学算法实现，效率比较高！欢迎大家下载学习！(matlab and vc6.0 achieve mixed programming source code, you can call C++ implementation matlab math methods, and do not need to install matlab, mathematical algorithms can achieve rapid implementation, more efficient! Welcome everyone to download study!)

DoA estimation with Concentric Circular Array

采用平面波展开法模拟2维光子晶体的能带结构,FDTD法模拟2维光子晶体能量传输(used plane wave expansion method for simulation of two-dimensional photonic crystal structure of the band, FDTD simulation of two-dimensional photonic crystal energy transmission)

Rayleigh in MRC scheme

A good matlab code that analysis the ROC curve and corresponding AUC value to estimate the sensitive and the currectness of the sample estimate. This code is suitable for variable type and function data.

编程仿真连续小推力实现GTO到GEO的三阶段转移过程，其中推力器的推力大小为0.8N，轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度，近地点角距为90度。 GTO轨道： ph:185km，ah：35786km，i：28.5°，GEO轨道：h：35786km，i：0°。 卫星质量为6600kg，从GTO到GEO，采用5000s的推力器。取地球半径为6378km，g取值为9.8m/s^2(The three stage transfer process from GTO to GEO is realized by simulation and continuous small thrust. The thrust of the thruster is 0.8N, and the starting point of orbital maneuver is the apogee of GTO. GTO orbit RAAN is 0 degrees, 90 degrees for the argument of perigee. GTO orbit: ph:185km, ah:35786km, i:28.5, GEO orbit: h:35786km, i:0. The mass of the satellite is 6600kg, from GTO to GEO, using the 5000S thruster. The radius of the earth is 6378km, and the value of G is 9.8m/s^2)