搜索资源列表
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
GPS_satellite_positions
- 推算GPS卫星24小时内的位置，matlab程序，本人花了很多时间编写！-projections GPS satellite within 24 hours of the location of Matlab procedures, I spent a lot of time to prepare!
sat_code
- 卫星计算码，对卫星位置结算有用，可以进行参考
quicklook
- 用idl开发的实现显示卫星图片在地球上位置的程序
Point Position.rar
- 能实现GPS伪距单点定位，包括文件的读写、误差改正、卫星位置、钟差的计算，以及最终伪距定位的实现。误差在10m以内,Can achieve single-point pseudorange GPS positioning, including reading and writing files, error correction, satellite position, clock bad calculation, and finally achieve pseudorange position
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.
gpsfangzhen
- 对GPS初学者来说，可以直观的查看GPS卫星分布以及进行模拟结算用户位置-Pairs of GPS for beginners, this may be an intuitive view to simulate GPS satellite distribution and settlement of user location
UKF
- GPS定位采用UKF滤波方式。包括调用的数据dat文件（选用卫星数据和机动目标运行轨迹数据）和调用的sigma点生成子程序。运行可观察定位误差（位置、速度和加速度）-GPS positioning using UKF filtering method. The data include call dat file (optional operation of satellite data and maneuvering target trajectory data) and the sigma
GDOPCalc
- 通过卫星坐标和测站位置计算三星DOP值，算法程序经略微改正也可用于多星DOP计算。-Satellite coordinates and the position of measurement calculated Samsung DOP value, the algorithm procedure can also be used by a slight correction of multi-satellite DOP calculation.
GPS-positioning--source-code
- 利用差分参考站和用户相对于导航卫星位置不同,引起了电波穿越电离层处的垂直TEC和角度不同是产生这种残差的主要原因,提出了一种改进的伪距差分算法并给出了定位算法。-Using differential reference station and the user with respect to the different navigation satellite position, causing the radio wave through the ionosphere at vertical
gpsPV
- 根据导航电文计算GPS卫星的位置和速度,并输出全部中间变量和最终结果-compute the position and vilocity of the GPS satellite
erti
- 二体问题是根据牛顿万有引力定律计算卫星轨道位置的计算方法，求取卫星六个轨道参数，应用于导航定位。-wqfrh wqrijqi qwiqd qwjrfhq qajwdqhi quqi sjfo fgiei dfafoif effwe qfefqqnfdqf sofqwofff lfkqq fwpfqkwkq fkqf
gps-satellite-position-calculation-
- gps卫星位置计算的程序，精确确定卫星的位置-gps satellite position calculation procedures to accurately determine the position of satellites
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.
satellite_situation_calculate
- 用c语言编写的用于计算gps卫星位置的一段程序，不是很难，主要是c语言-Using c language a program used to calculate the gps satellite position is not difficult, mainly c language
gpsPosition
- GPS定位程序 内含rinex数据文件 计算导航卫星位置，接收机位置等 同时包含word说明和精度结算-GPS positioning data file containing rinex calculate navigation satellite position, receiver position, etc. contain word descr iptions and precision settlement
try.cpp
- 根据gps导航电文计算卫星位置x，y，z坐标，c++程序-According gps navigation message to calculate satellite position
Calculated-the-satellite-position
- 由卫星星历计算卫星位置，是由c#语言编写，有简易的界面，公式准确，已验证过正确性-Calculated by the satellite ephemeris, the satellite position, is written by c# language, has a simple interface, accurate formula, correctness has been verified
coe_from_rv1
- % 此函数由初始轨道的位置和速度矢量轨道参数 % %参考资料: % Howard D.Curtis 《Obital Mechanics for Engineering Students》 % P158-164 4.4 Orbital elements and the state vector % 参考代码：P606-608 D.8 coe_from_sv.m %常量： % mu -
卫星位置计算
- 先给定初始常数值后，通过迭代计算偏心异常、计算升序节点和格林威治子午线之间的角度来计算卫星的位置，并给出计算卫星速度的方法。(After the initial constant is given, the position of the satellite is calculated by iterating the eccentricity anomaly, calculating the angle between ascending node and Greenwich meridian