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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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<strong>Inter</strong> <strong>Satellite</strong> <strong>Links</strong>Simulations <strong>and</strong> ResultsRadial Error [cm] 1998 07 02 14:35 - 1998 07 04 02:3510.0-10.00[h]5 10 15 20 25 30 35Along Track Error [cm] 1998 07 02 14:35 - 1998 07 04 02:3579.0-79.00[h]5 10 15 20 25 30 35Cross T rack Error [cm] 1998 07 02 14:35 - 1998 07 04 02:355.0-5.00[h]5 10 15 20 25 30 35Figure 6-42 MEO propagation error with 6 hour smoothingThe along track error also shows a secular error tendency, but much smaller than that of thepropagated raw estimate. If the same broadcast model is fit over this propagated orbit, theURE remain below 30 cm even nearly up to 24 hours, as can be seen in the following picture.R. Wolf Page 141

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