ACA-radar-Overview

基于matlab GUI做的单位换算器，实现多种单位的一次性换算(Unit converter made of MATLAB GUI)

VC_Matlab air conditon主要讲述了基于VC 和Matlab环境下的空调设计方案(VC_Matlab air conditon mainly about VC and Matlab environment based on air-conditioning design)

说明：  多变量丢翻图方程的求解程序，编写简单，直接运行M文件(diophtine)

mimo clutter space time steering vector

利用MATLAB的GUI功能制作电机旋转磁场演示软件。(MATLAB-GUI features making use of the motor rotating magnetic field presentation software.)

安卓开发实战读物！带领你做工程！由Mark Murphy大师编著(Andrews developed real books! Lead you to do works!)

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)

3个matlab原程序文件，包括： 1-32是：图形应用篇 33-66是：界面设计篇 67-84是：图形处理篇 85-100是：数值分析篇 (three Matlab original files, including : 1-32 : Graphics Applications articles 33-66 is : interface design articles 67-84 is : graphics processing Chapter 85-100 is : Numerical Analysis Section)

蔡氏电路MATLAB仿真程序，分析，绘图，手动设置参数(Chua' s circuit simulation program MATLAB, analysis, mapping, set the parameters manually)

synchronious machines