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Description: 读取Rinex格式星历文件，包括对星历的搜索，以及星历更新的判断-Rinex read format ephemeris documents, including the ephemeris search, and update the ephemeris judgment
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Size: 15739 |
Author: 张家 |
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Description: 关于GPS星历的一些常用的算法。本文件无接压密码，直接用RAR解压即可。-GPS ephemeris of the commonly used algorithms. Without access to this document password pressure directly RAR decompression can be used.
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Size: 4509 |
Author: 张家 |
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Description: 根据GPS卫星的广播星历，计算卫星的位置，也可以进行GPS卫星位置的预报-GPS satellite broadcasting ephemeris, the location of the satellites, will be able to conduct the GPS satellite location prediction
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Size: 138064 |
Author: 付建红 |
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Description: 计算卫星星历的小程序，还不太完善，请多多指教。VC++6.0环境下编译-satellite ephemeris calculation of the small program is not really perfect, the exhibitions. VC 6.0 compiler environment
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Size: 34011 |
Author: 任玉川 |
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Description: 龙格库塔算法，用于拟合GLONASS的星历数据，15分钟精度在5米之内，可以向前推，也可以向后推！-Runge - Kutta method for fitting the GLONASS satellite ephemeris data, the accuracy of 15 minutes within five meters, can move forward, but also can push back!
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Size: 29375 |
Author: 于兴旺 |
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Description: GPS星历内插资料,分别采用拉格朗日,牛顿法,是不错的资料!-GPS ephemeris data interpolation, using Lagrange, Newton's Law, which is good information!
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Size: 215996 |
Author: 于兴旺 |
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Description: 用于GPS卫星的位置和速度解算，输入的参数为卫星的星历及所要计算的时刻-GPS satellites for the position and velocity solution, the input parameters for the satellite ephemeris and to calculate the moment
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Size: 1503 |
Author: 谢鹏 |
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Description: 根据卫星星历及测者位置，判断卫星是否可见-satellite ephemeris and location were measured to determine whether the satellite can be seen
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Size: 8871 |
Author: 张广星 |
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Description: 读取Rinex格式星历文件，包括对星历的搜索，以及星历更新的判断-Rinex read format ephemeris documents, including the ephemeris search, and update the ephemeris judgment
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Size: 15360 |
Author: 张家 |
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Description: GPS数据处理源代码，提供了星历处理、伪距定位、载波定位的函数。-GPS data processing source code, provided ephemeris treatment, pseudo-range positioning, carrier positioning function.
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Size: 116736 |
Author: liran |
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Description: 读取renix格式的卫星星历文件，支持原始网络下载文件，阿紫泰克软件转换的星历文件，将数据存在数组中待计算-Read format renix satellite ephemeris files, support for the original network to download documents, Tektronix阿紫conversion software ephemeris file to the data array to be calculated
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Size: 1024 |
Author: huangjie |
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Description: gps GPS matlab GPS lab ephemeris.m matlab gps toolbox gps toolbox Software Receiver
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Size: 1991680 |
Author: Ivan |
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Description: GPS单点定位源码，包括读观测，广播星历文件，精密星历文件，对于要学习GPS算法编程的人是极好的资料哦-GPS single point positioning source, including the time observation, broadcast ephemeris file, precise ephemeris files for the GPS algorithm to learn programming is excellent information, oh
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Size: 368640 |
Author: yby |
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Description: 星历计算 可以自己调试运行下 很好的一个matlab程序 根据一本书编写的-Ephemeris calculation a good matlab programme
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Size: 2048 |
Author: zhoufucmt |
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Description: Convert WGS 84 (CTS, ECEF) Coordinates to ECI (CIS, Epoch J2000.0) Coordinates. This function has been vectorized for speed. The associated error in converting between coordinate frames is on the order of 1.2*10^-11 km when compared to STK ephemeris output.
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Size: 4096 |
Author: CYT |
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Description: 实现GPS原始星历数据的读取和转化为十进制的数据用于计算卫星的具体坐标和方向速度-To achieve the original GPS ephemeris data read and converted to decimal data used to calculate the satellite coordinates and direction of specific speed
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Size: 2048 |
Author: |
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Description: 运用给出的相关参数，设计一种巧妙计算出轨道参数及反算卫星星历的算法-Use of the given parameters, design an ingenious algorithm calculate the orbital parameters and Inverse satellite ephemeris
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Size: 3695616 |
Author: 老男孩 |
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Description: 利用瞬时轨道参数计算协议地球坐标系及相关坐标系下的卫星星历，C# 控制台程序。-Satellite ephemeris calculation of earth coordinate system protocol and relative coordinates using instantaneous orbit parameters, a C# console application.
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Size: 34816 |
Author: 张洛恺 |
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Description: 通过轨道根数的计算，解算星历二体问题的状态向量-By orbital calculation solver ephemeris two-body problem of the state vector
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Size: 2048 |
Author: 连月勇 |
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Description: 通过对GPS星历提供的卫星位置坐标，拟合出定位卫星坐标所需要的15个参数，利用拟合出的参数对接下来的时间对卫星位置进行定位-GPS location coordinates via satellite ephemeris provided for fitting the 15 parameters required positioning satellite coordinates, using the fitted parameters the next time the position of the satellite positioning
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Size: 3222528 |
Author: liu |
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