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Satellite Orbit Computation 1.0

 
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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.

Tags: Collected, Structure, Retained, Subsequent, Outputs, Velocities, Constant, Altitude, Intercepts, Display

Platforms: BSD , Mac OS X , Solaris , linux

 
Added: 25 February, 2013 06:13 File size: 747.5 KB
Status: new Download times: 512 kb/s: 12 s
Program type: shareware   1 Mb/s: 06 s
      2 Mb/s: 03 s
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Tags: Collected, Structure, Retained, Subsequent, Outputs, Velocities, Constant, Altitude, Intercepts, Display

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