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fiber-TE-mode
利用matlab模拟光纤中TE模的模式分布图。(Using matlab simulation model TE mode fiber distribution.)
- 2013-07-30 10:05:34下载
- 积分：1
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openGL
分别用普通构建方式和显示列表对物体进行绘制，实现各种复杂的交互控制(Were built with ordinary ways and display a list of objects to draw, to achieve a variety of complex interactive control)
- 2014-02-17 20:00:17下载
- 积分：1
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MATLAB_VCPP
详细介绍了MATLAB与VC混合编程的几种方法，并给出了十分详细的配置步骤和安装方法，亲测可用。(Details of the several methods of MATLAB and VC mixed programming, and gives a very detailed configuration steps and installation methods, pro-test available.)
- 2014-08-18 10:34:51下载
- 积分：1
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BasicTime
You all might have used CTime or CTimeSpan to manipulate the system timer. Here is an article to show you how your system timer works. I will give you an idea of port communications behind the system clock manipulations. Those who are a little biased on hardware and software interfacing practices would find this article of great help.
- 2007-10-16 09:37:44下载
- 积分：1
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high-pass-filter-matlab-
三维数字滤波器中的理想高通滤波器的matlab仿真及其结果(3 d digital filters in an ideal high-pass filter matlab simulation and the result)
- 2011-12-13 15:41:24下载
- 积分：1
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guass_call_c
说明： 光斑聚集的C++程序调用，以前MATLAB计算要15分钟，现在只要3分钟就可以算完。运算超快。(Gathering spot called C++ program, MATLAB calculations to 15 minutes, now only 3 minutes. Ultrafast operation.)
- 2011-04-13 17:29:36下载
- 积分：1
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ImageSolarize
image solarizing processing(image processing solarizing)
- 2007-07-10 22:32:24下载
- 积分：1
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MATLAB5
小波分析尺度函数，样条数据处理，梁的有限元分析(Wavelet scaling function5)
- 2011-12-20 19:03:16下载
- 积分：1
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binary
C program of binary search
- 2015-03-06 14:58:59下载
- 积分：1
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han1
这里我们针对三级固体火箭进行研究，主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差（相差 ）时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中，火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行，第二、三级飞行时已在大气层外，此时可忽略气动力的影响。(Here we study for three solid rocket, the main consideration at every level when the engine thrust and state arising the moment the rocket off point perturbation deviation (difference) in the presence of specific impulse and engine test bias. Outside of the rocket flight dynamics equations can be established on the ground coordinate system launch, the rocket s first stage, the second and third stages according to a fixed elevation angle of flight procedures, and the second, when the third flight already in the atmosphere, this when can ignore the effects of gas dynamics.)
- 2020-11-03 20:39:53下载
- 积分：1
