📄 contents.m
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%GPS Toolbox
%Version 1.0 17-Oct-1997
%
%Directory: bancroft
%
%ABS_POS Script for calculating an absolute position of a receiver.
% Input is 4 or more pseudoranges for the Bancroft algorithm,
% a list of satellites and received time
%
%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.
%
%BANCROFT Calculation of preliminary coordinates for a GPS receiver
% based on pseudoranges to 4 or more satellites. The ECEF
% coordinates (see function e_r_corr) are the first three
% elements of each row of B. The fourth element of each
% row of B contains the observed pseudorange. Each row pertains
% to one satellite. The pseudorange in the first row of B is
% used to discriminate between the two possible solutions.
%
%CHECK_T repairs over- and underflow of GPS time
%
%E_R_CORR Returns rotated satellite ECEF coordinates due to Earth rotation
% during signal travel time
%
%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.
%
%K_POINT Prepares input to the Kalman algorithm for finding the final
% position of a receiver. The inputs are preliminary station
% coordinates calculated by a call of b_point (Bancroft algorithm),
% pseudoranges, prn's, and measurement received time.
%
%KLEUS Explicit method for computing preliminary receiver coordinates
% from four pseudoranges and ECEF coordinates of four satellites
%
%LORENTZ Calculates the Lorentz inner product of the two 4 by 1 vectors
% x and y
%
%NORMALS Accumulates the contribution of one observation equation and
% adds it to the coefficient matrix AtA and the right side AtY.
% The accumulated result is outputted under the same name.
%
%SATPOS Calculation of X,Y,Z coordinates at time for given ephemeris
% eph
%
%TOGEOD Subroutine to calculate geodetic coordinates latitude,
% longitude, height given Cartesian coordinates X,Y,Z, and
% reference ellipsoid values semi-major axis a and the inverse
% of flattening finv.
%
%TOPOCENT Transformation of vector dx into topocentric coordinate
% system with origin at X. Both vectors are 3 by 1.
% Output: D vector length in units like the input
% Az azimuth from north positive clockwise, degrees
% El elevation angle, degrees
%
%TROPO Calculation of tropospheric correction. The range correction ddr
% in meter is to be subtracted from pseudo-ranges and carrier
% phases
%%%%%%%%%%%%%% end contents.m %%%%%%%%%%%%%%%%%%%%%%%%%%%%
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