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satellite
- 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
AccBiasCarousel
- GPS的卫星星历$RGEA 983 181267.50 14 B00FF 2 21239223.084 0.051 -111612873.189 0.004 65.980 50.7 1066.340 83E14 2
BrdCasPos
- 利用广播星历计算卫星轨道坐标，间隔15分钟
sp3abstract
- 对SP3精密星历的某颗卫星的X坐标进行提取，组成新的观测文件
读取广播星历
- 用于读取gps接收机的广播星历文件
glonassPpvt
- GLONASS单点定位程序，可以根据卫星星历解算地面点坐标。-According GLONASS ephemeris files, calculate GLONASS satellite coordinates.
TLE
- 关于TLE两行星历的数据读取的模型，便于卫星的定位等处理-TLE two planets on the calendar to read the data model, easy to deal with satellite positioning
SPP
- 根据GPS卫星观测文件（.00O）与星历文件(.00N)，计算各历元测站的位置。-According to documents GPS satellite observations (.00 O) and ephemeris file (.00 N), calculated each epoch station location.
sv
- 根据卫星星历和时间数据计算卫星在天球坐标系中的坐标。-Based on satellite ephemeris and time data of the satellite coordinates of the celestial coordinate system.
2008302590115
- 根据星历文件算卫星坐标。。这是我们实习用的。绝对正确-Calculated according to the satellite coordinates of the ephemeris file. . This is our practice to use the. Absolutely right
GPS-satellite-track
- 以GPS卫星为例，主要介绍利用SDP8模型，预报GPS卫星在几天内的星历，从而利用BorlandC++Builder 编程实现GPS卫星星座、星下点轨迹仿真及全球DOP值图形分析，测站星空图变化，测站DOP值分析，从而更好的分析GPS卫星星座、轨道变化、卫星的性能, 为改进卫星的星座及轨道提供技术依据。-This paper introduces that is using SDP8 propagation model to predict GPS of position and velocit
gps
- GPS卫星坐标计算，通过卫星星历表数据的参数传递来计算卫星坐标-GPS satellite coordinates calculated parameters passed via satellite ephemeris data to calculate the satellite coordinates
GPSSatCalc
- GPS星历文件解算。包括，将世界时转换为GPS时和读取星历文件中的数据并存储等。-The GPS ephemeris File solver. Including conversion for GPS and to read the ephemeris file data storage.
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
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
GPSSatellitePosition
- 该程序的主要功能是利用卫星星历解求卫星位置。-The program' s main function is to seek solutions using satellite ephemeris satellite position.
Application
- 星历计算，通过两个观测历元来计算卫星的轨道参数-Ephemeris calculations by two epoch observations to calculate the satellite orbit parameters
orbital-elements
- 卫星轨道参数正反算，根据卫星的位置和速度，求取实时卫星轨道的两行根数，即6个开普勒根数。卫星星历计算以及卫星轨道参数计算-Considered the pros and cons of satellite orbit parameters, depending on the location and speed of the satellite, two lines of strike root of the number of real-time satellite orbit that Ke
attitude-determination-with-GPS-
- 多天线姿态确定工具箱，包括星历读取、单点定位、差分定位、坐标转换、定姿等-In this paper a MATLAB toolbox for determining the attitude of a rigid platform by means of multiple non-dedicated antennas using global positioning system is presented. The programs embedded in this toolbox cover