Apartment_Management

说明：  实现ASK DPSK 调制解调的matlab 仿真(to come true ASK DPSK)

本文主要是维纳滤波器的设计，包含设计内容(This article is mainly Wiener filter design, including the design of content)

本程序可以用来计算太阳能总辐射，晴天模型(simulation the total solar radiation)

本程序用于判别所给数据源在置信率为0.05时的概率分布形式。A的形式为n×1。(This procedure is used to determine the distribution of the given data source in the form of confidence was when the probability of 0.05. Form A is n × 1.)

通过matlab程序实现，基于光流法的运动估计，可以对图像进行预测(By matlab program, optical flow motion estimation method based on the image can be predicted)

matlab coding about up and down sampling(up and down sampling)

雷达基础导论，雷达监测，雷达波形，雷达模糊函数，脉冲压缩，面杂波与体杂波，动目标显示和杂波抑制，相控阵，目标跟踪，电子对抗，雷达截面积，高分辨率战术合成孔径雷达，信号处理。(MATLAB Simulation for Radar System Design)

mo phong matlab quy dao robto mon hoc robo cong nghiep

说明：  Adding Two different matrecis with the same dimentions by matlab

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)