GPS Toolbox matlab

 include • Principle of Radio Navigation: navigation base on trilateration has been investigated and the over determined Eq. for navigation has been solved.   • GPS Ephemeris Data: for GPS navigation, the position of GPS satellite is very important so the by receiving ephemeris data the position of the satellite is determined.   • GPS Errors: Three different sources of errors in GPS navigation has been investigated (Ionosphere, Troposphere and Satellite clock). Ionospheric Error model is generated base on Parkinson [1] and the Tropospheric Error Model based on Hopfiel model [2].   • Simulation & GPS Toolbox: One of the targets of this work is generating MATLAB GPS Toolbox and in one case study the performance of generated toolbox will be verified.

Calc_Azimuth_Elevation.m
Distance.m
ECEF2GPS.m
Error_Ionospheric_Klobuchar.m
Error_Satellite_Clock_Offset.m
Error_Satellite_Clock_Relavastic.m
Error_Tropospheric_Hopfield.m
Gen_G_DX_XYZ_B.m
GNT08.1.2.docx
Kepler_Eq.m
main.asv
main.m
manulaGNT08.1.2.pdf
plot_Orbit.m
project_data.mat
SV_Ephemeris_Model.m
XYZ2ENU.m