搜索资源列表
sc
- 根据广播星历，计算GPS卫星坐标，星历文件需要预处理-sv coordinate calculation
GPS
- 本次编程内容是利用卫星星历计算卫星不同时刻所在位置的计算。-The programming content is to use the location of the satellite ephemeris calculation satellite different time calculation.
GPS-single-point-positioning
- GPS单点定位程序，采用C#编程，导入星历文件，可实现GPS单点定位计算-GPS single point positioning procedures, using C# programming, import ephemeris file, GPS single point positioning calculation
IGS
- RTK相位测量 读IGS精密星历子程序 RTK程序初步设计-RTK phase measurement reading IGS precise ephemeris subroutine RTK Program Preliminary Design
GPSXingliCal
- 通过GPS广播星历计算卫星坐标，返回每一个时刻的卫星在地固坐标系中的坐标。-Calculated by the GPS broadcast ephemeris satellite coordinates, return every moment of satellites in earth-fixed coordinate system coordinates.
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
GPS
- 用广播星历计算卫星位置Calculation of GPS satellite position using broadcast ephemeris-Calculation satellite position using broadcast ephemeris
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
pr_gps
- 学习gps重要的资料，卫星星历是仿真的，计算方法为卡尔曼滤波，包含速度参数-Learn gps important data, satellite ephemeris is simulation, computational methods for the Kalman filter, including the speed parameter
ephemeris-two-body
- 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
readnavfile
- 很好的一个程序，读取gps卫星星历的，很简单，有助于初学者学习。-A very good program, read gps satellite ephemeris, very simple to help beginners learn.
RinexNFile
- 一次性读取Rinex 2.1格式广播星历文件所有内容的类实现-Read content of broadcast ephemeris file (Format: Rinex 2.1) all by once
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
EarthToMars
- 应用matlab语言，应用lambert变轨实现地球到火星的发射窗口的轨道寻优。内涵lambert变轨功能，星历计算等多个函数文件-Application of matlab language, application lambert achieve orbit the Earth to orbit Mars launch window optimization. Connotation lambert orbit function, ephemeris calculations and oth
Ephemeris_And_Orbital
- 利用卫星的星历参数计算其轨道，同时还能根据速度和加速度反算星历参数，是基于MFC对话框的编程-Using satellite ephemeris parameters to calculate its orbit, while depending on the speed and acceleration of the inverse ephemeris parameters is based on MFC dialog programming
satnav3
- 卫星导航工具箱3.0.可以计算伪距、各种GPS误差、卫星星历等等。-SATNAV3 TOOLBOX FOR MATLAB
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 precision ephemeris read, Hopfield m
OrbitDynamics
- 卫星轨道动力学的解算，如轨道根数的求解，星历计算等。-Satellite orbital dynamics solver, such as orbital solving
get_Ephemeris
- 获得导航电文中的各卫星的星历数值，并存到矩阵eph中-For navigation message of each satellite ephemeris values coexist in the matrix eph
weixingdingwei
- 作者在学习《航天系统》时，在c++6.0环境中实现的卫星定位的算法程序。包括通过轨道根数求卫星状态参数的算法和通过卫星状态参数反求卫星星历的算法。-Author of the study "space system" is in c++6.0 environment to achieve the satellite positioning algorithm. Including through the orbital parameters of the algorithm for the sa