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精密星历文件读取
- 实现对精密星历数据的读取,并能内插出任意时间点卫星的位置,且能评定内插的精度.-to achieve precise ephemeris data to the reader, and interpolation from any point in time the satellite location and can assess the accuracy of interpolation.
精密星历文件读取
- 实现对精密星历数据的读取,并能内插出任意时间点卫星的位置,且能评定内插的精度.-to achieve precise ephemeris data to the reader, and interpolation from any point in time the satellite location and can assess the accuracy of interpolation.
readigs
- 读取精密星历文件，方便快捷，代码简单易懂-Read precise ephemeris file, convenient, easy to understand code
SP3Read
- C# GPS中精密星历文件的读取，编程引用很方便，节约时间-C# GPS in precise ephemeris file read, programming references is very convenient, saving time
RinexSp3File
- 一次性读取Rinex格式精密星历文件所有内容的类实现-Read content of precise ephemerise file (Format: Rinex) all by once
GPS_SPP
- GPS伪距单点定位，包括导航文件、观测文件、精密钟差和精密星历的读取，对流层Hopfield模型，电离层K8模型，采用最小二乘法，最后通过调用matlab来计算测站坐标。对GPS编程初学者是很好的编程哦。-GPS pseudorange point positioning, including navigation documents, observation files, precision clock bias and precis
read_SP3
- 本程序用于读取GPS中精密星历SP3文件，得到各个卫星的坐标序列-read the sp3 file of GPS
matlab-files-of-GPS
- 读取IGS文件（观测文件*.*o 广播星历*.*n；精密星历*.sp3；修正电离层对流层）。均是matlab函数形式，可直接用于GPS matlab数据处理-reading IGS files (oberservation file*.*o navigation files*.*n precise orbit*.sp3) correct errors of Ionosphere delay and Tropsphere delay
RinexSp3Reader
- 读取GNSS卫星精密星历Sp3文件。传入精密星历文件地址，便可以进行精密星历数据读取，读取完成后按卫星、时间、X、Y、Z格式存储在表结构中，以表的形式返回以供使用。-Reads the GPS satellite precise ephemeris Sp3 file. Incoming precise ephemeris file address, you can read the ephemeris data. Read as for
satellite-position
- 读取sp3文件（P类型）中的精密星历，并用拉格朗日多项式九阶内插法计算卫星位置-Sp3 read the file (P type) in the ephemeris, and calculates the satellite position with a ninth order Lagrange polynomial interpolation
SP3clk
- 读取精密星历文件、还可获取不同采样率的钟差差值结果，如30s，300s。(Read the precise ephemeris file and get the difference between the clock difference of different sampling rates, such as 30s, 300s.)
satellite-position
- 首先根据卫星PRN号读取精密星历文件内容，然后通过朗格朗日内插计算出卫星的位置，里面含有sp3文件和exe程序(First read the contents of the precise ephemeris file according to the satellite PRN number, and then calculate the position of the satellite by Lange Lange interpo