资源列表
CC2NONCC_ESOCv6.2
- cc2noncc,gps算法中dcb改正模型，如无法打开，请将后缀名改为tar.-cc2noncc, gps algorithm dcb correction models, such as can not be opened, add the suffix name was changed to tar.
Bernese
- gps定位软件bernse的使用说明，比较少见-gps navigation software bernse instructions for use, are relatively rare
GPS
- GPS Demo, demo gps chinese
GPS_Speci
- 详细的GPS测量规范，对从业人很有参考价值-GPS measurement of the detailed specifications of great reference value for Practitioners
UnderstandingGPSPrinciplesandApplications2ndKaplan
- GPS ebook for understanding GPS archietecture
GPS_path_tracker
- GPS路径跟踪记录器扩展(通过Web服务在SQL2005中存储路径)-GPS Path tracker recoder
alm2pos
- ALM2POS computation for satellite position from almanac data file [pos,R]=alm2pos(almanac,PRN,time) calculates the satellite position in the Terrestial and in the Celestial reference frame for a desiderate satellite vehicle (PRN) with alm
avspos
- AVSPOS extracts the available satellite position (XYZ) XYZ=avspos(X,Y,P1,P2) extracts the visible satellites, which are described in P2, from the matrix X. The output XYZ is a N-by-3*M matrix with the coordinates of the visible satellites.
alm2skyplot
- ALM2SKYPLOT is a program for the satellite constellation [PRN,XYZ,T]=alm2skyplot(DoW,St,Et,I,P,file) is a program which calculates the GPS satellite positions from an almanac file and makes a skyplot (satellite-elevation-plot) for the desi
skyplot
- SKYPLOT for a given receiver position Y=skyplot(X,PRN,C,O) draws the skyplot for the receiver position. The required inputdata for the calculation of the skyplot X is N-by-3*M matrix, where N are the timesteps and M is the number of the Sat
almIN
- ALMIN Import for Almanac Datafiles almanac=almIN(alm_file) import almanac Files in YUMA-Format. The name of the file can be choosen by naming the File as Input parameter or by choosing the file manually (NO INPUT needed).- ALMIN Import fo
elevat
- ELEVAT calculation for elevation, zenit angle and spatial distance e_az_s=elevat(D,RHO) computes the elevation, the zenit angle and the spatial distance between a satellite(j) and a receiver(i). The receiver position (D) is a 3-by-3 matrix