%GPS Toolbox %Version 1.0 17-Oct-1997 % %Directory: ash_base % %ASH_BASE Estimation of ambiguities by sequential least squares. % Goad's "60-77 Algorithm" determines the final values % of ambiguities. Finally, estimation of vector follows. % During estimation ionospheric delay is set to zero. % %ASH_DD Arrangement and formatting of double differenced code % and phase observations. % %B_POINT Prepares input to the Bancroft algorithm for finding % a preliminary position of a receiver. The input is % four or more pseudoranges and the coordinates of the % satellites. % %BDATA Reorganization of binary P-code data as resulting % from Z-12 receiver. Input of b-files from master and rover. % Typical call: bdata('b0810a94.076','b0005a94.076') % %EDATA Reads a binary ephemeris file and stores it in % a matrix with 21 rows; column number is the number of % ephemerides. % Typical call: edata('e0810a94.076') % %FIND_EPH Finds the proper column in ephemeris array % %GET_EPH The ephemerides contained in ephemeridesfile % are reshaped into a matrix with 21 rows and % as many columns as there are ephemerides. % %GET_RHO Calculation of distance in ECEF system between % satellite and receiver at time tR_RAW given the % the pertinent ephemeris Eph. % %K_DD3 Kalman Filter for Estimation of Ambiguities (with I = 0) % Double differenced code and phase observations % SV is the satellite to be differenced with ref. sat. 26. % The choices are: 2, 9, 16, 23, 27 % %K_DD4 Kalman Filter for Estimation of Ambiguities % Double differenced code and phase observations % %SATPOS Calculation of X,Y,Z coordinates at time t % for given ephemeris eph % %SDATA Reading of antenna offsets. The 2 antenna heights are saved % as h = ["rover"; "master"] % Typical call: sdata('s0810a94.076','s0005a94.076') % %TOGEOD Calculate geodetic latitude, longitude, height given % Cartesian X,Y,Z, and reference ellipsoid values % semi-major axis (a) and the inverse flattening (finv). % %TROPO Calculate tropospheric correction. The range correction ddr % in meter is to be subtracted from pseudo-ranges and carrier % phases. %%%%%%%%%%% end contents.m %%%%%%%%%%%%%%%%%%%%%%%%