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Satellite Orbit and Ephemeris Determination using Inter Satellite Links

Satellite Orbit and Ephemeris Determination using Inter Satellite Links

Satellite Orbit and Ephemeris Determination using Inter Satellite Links

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Autonomous Onboard Processing<strong>Inter</strong> <strong>Satellite</strong> <strong>Links</strong>7.4.3.3 Clock DriftThe third case simulates a sudden excessive drift of 10 -10 sec/sec in the clock of SV 04, whichis visible to the user at a high elevation. The figures below indicate true <strong>and</strong> estimation errorof the onboard processor.1,41,21,00,8XYZTError [m]0,60,40,20,0-0,212:01:24.000 12:01:49.000 12:02:14.000Time [hour:min:sec]Figure 7-18 Absolute Clock Error SV 040,05dXdYdZdT0,00-0,05Error [m]-0,10-0,15-0,2012:01:24.000 12:01:49.000 12:02:14.000Time [hour:min:sec]Figure 7-19 Estimated vs True Error SV 04Page 182R. Wolf

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