滤波法

将icrs坐标系转换到ITRS坐标系。matlab代码(ICRS to ITRS transformation)

COM+TCP控制作。功能强大，拿去测试(COM+TCP u63A7 u5236 u4F5C u3002 u529F u80FD u5F3A u5927 uFF0C u62FF u53BB u6D4B u8BD5)

用于激光扫描的RTC5振镜控制的DLL、LIB和头文件(DLL, LIB and header files for the control of RTC5 galvanometer for laser scanning)

自己辛苦编写的双色球彩票统计预测程序. 为得到下载积分,忍痛贡献. visual c++ 2010, 开发. windows 7 64bit, 16GByte内存需求, 4核处理器 并行计算, STL C++, 能够快速遍历计算全部号码分解组合的概率. 贡献出来心痛. 希望联系我,找份喜欢的工作.(souce codes of double Color ball lottery statistical forecasting program, desinged by myself. visual c++ 2010 stl, parallel computing. operation requirement under windows 7 64bit, 16GByte memory and 4-core processor. Rapidly traverse calculation of the the probability of all decomposition and all combination code numbers. it have me heartache to contribute my codes for get download points. Hope to contact me, help me ge one job.)

说明：  地震数据反演处理软件，程序ANRAY95是汉堡大学地球物理研究所Gajewski和Psencik等编写的ANRAY86和ANRAY89的修改版本,适用于用射线的方法数值模拟三维各向同性或各向异性介质中地震波场传播问题。 (Inversion of seismic data processing software, the program is ANRAY95 Institute of Geophysics, University of Hamburg Gajewski and Psencik prepared ANRAY86 and ANRAY89 such as a modified version of the method applied to numerical simulation using ray three-dimensional isotropic or anisotropic media in the dissemination of seismic wave field问题.)

ansys计算转子轴系临界转速，画坎贝尔图的源代码(ansys rotor shaft critical speed calculation, painting Campbell diagram of the source code)

this is a guidle for cnc machine

《测量平差程序设计》（宋力杰编著）一书的源码(" Surveying Adjustment Program Design" (Song Lijie eds) source)

说明：  Matlab显式三维地震数据的源代码，从事地震勘探研究的同行可下载，很方便(Matlab explicit three-dimensional seismic data of the source code, engaged in seismic research peer can be downloaded, it is convenient)

这是我在CSDN上找到的比较好的一个关于卫星轨道动力学的一个源码包，简单易懂，用c++写的，作者是韩冬，向他致敬！ 非常好用的程序，学习卫星轨道动力学(This is I find in good CSDN about the dynamics of the satellite s orbit a source packages, easy to understand and use c++ written, the writer is HanDong, paid tribute to him! The program is very nice, learning satellite orbit dynamics)