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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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Simulations <strong>and</strong> Results<strong>Inter</strong> <strong>Satellite</strong> <strong>Links</strong>6.2.3.2 Ground <strong>and</strong> <strong>Inter</strong>satellite TrackingIn this scenario, intersatellite links provide also an enhancement in accuracy similar to theIGSO Walker constellation.Radial Error [cm] 1998 07 02 08:59 - 1998 07 11 02:5930.0Radial Std. Dev. [cm] 1998 07 02 08:59 - 1998 07 11 02:5915.010.0-15.005.0-30.0[h]50 100 150 2000[h]49 98 147 196Along Track Error [cm] 1998 07 02 08:59 - 1998 07 11 02:5934.0Along Track Std. Dev. [cm] 1998 07 02 08:59 - 1998 07 11 02:5917.022.0-17.0011.0-34.0[h]50 100 150 2000[h]49 98 147 196Cross T rack Error [cm] 1998 07 02 08:59 - 1998 07 11 02:5928.0Cross T rack Std. Dev. [cm] 1998 07 02 08:59 - 1998 07 11 02:5914.024.0-14.0012.0-28.0[h]50 100 150 2000[h]49 98 147 196Figure 6-23 Tracking Accuracy of IGSO on a Loop with Custom Global Network <strong>using</strong>additional ISL'sPage 118R. Wolf

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