This program includes of
•Principle of Radio Navigation Calculation: 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 and the Tropospheric Error Model based on Hopfiel model.
•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
moein mehrtash (2021). GPS Navigation Toolbox (https://www.mathworks.com/matlabcentral/fileexchange/41364-gps-navigation-toolbox), MATLAB Central File Exchange. Retrieved .
Equations are wrong.
ex..) Error_Ionospheric_Klobuchar.m > t(i), F(i), T_iono(i) ....
Hi Moein. Chetori dadash? In SV_Ephemeris_Model function, you did not consider inclination in "function input format". In other words, your format is 15xN, while the function needs 16xN data. take a look at your manual (MANULA?) and revise it.
How did you incorporate iono error and tropo error and the user clock bias
how to obtain the values in project_data.mat especially pr? with calculation or another simulation tool?
how to take satellite position and receiver position values
where do we enter the Lat/Long to run the script? Is it the main.m?
How could I create a project_data.mat? Because I really don´t know the structure of this file and I would like to understand it.
Hi! This tollbox doesn't works in MatLab R2009b, so I find the mistakes and correct them. If this tollbox shows error, you may dowload corrected version from this link:
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