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Satellite Orbit Computation

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5.0 | 3 ratings Rate this file 85 Downloads (last 30 days) File Size: 745 KB File ID: #28888 Version: 1.3
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Satellite Orbit Computation

by

Charles Rino (view profile)

 

29 Sep 2010 (Updated )

Modified SGP4 code for GPS interface

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Description

A modified version of the SGP4 code used for standard satellite orbit computation using two-line elements (TLE). The modified code outputs satellite positions and velocity in ECF coordinates and universal time from EPOCH. Utilities are provided to calculate point-to-point angle, range rates, TCS positions, constant altitude intercepts and velocities. Outputs are collected in a structure and retained in a *.mat file for subsequent display and Beacon satellite data analysis applications. Documentation and examples are provided. Code uses GPS_CoordinateXform and IGRF utilities available from MATLAB Central.

MATLAB release MATLAB 7.11 (R2010b)
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Comments and Ratings (7)
15 Sep 2016 Matt Rebholz

I tried running the GenerateSatelliteGeometry_DEMO and I too cannot run it because of a missing file, ecf2llhT. Has anyone been able to get this to run? Thank you.

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25 Oct 2015 priya pawar

Where can I get MATLAB code

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24 Aug 2015 Anthony

Please retract the missing function comment. I had an error translating the pdf address in the readme file.

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24 Aug 2015 Anthony

I came up with a missing function on line 89?
ecf2llhT

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26 Jul 2015 HENRY XSCC  
04 Jul 2014 Lorenzo Luini

I would like to ask: in the sgp4 code, what are the units of the inputs? Also the code gives an error at line 151 because of the missing satellite number to be provided as input.
Thank you in advance!

07 Aug 2011 Junling Wang  
Updates
30 Sep 2010 1.2

Error corrected in function satGEOM. Only affects results that use magnetic field geometry.

18 Oct 2010 1.3

Corrected error in satGEOM utility. SGP4 is unaffected.

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