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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> Results6.2.3 IGSO on three Loops6.2.3.1 Ground TrackingThis scenario provides nearly as good tracking accuracy as the Walker constellation. Thedifferences result from the higher inclination of the orbits.Radial Error [cm] 1998 07 02 05:59 - 1998 07 09 17:5940.0Radial Std. Dev. [cm] 1998 07 02 05:59 - 1998 07 09 17:5920.040.0-20.0020.0-40.0[h]43 86 129 1720[h]42 84 126 168Along Track Error [cm] 1998 07 02 05:59 - 1998 07 09 17:5952.0Along Track Std. Dev. [cm] 1998 07 02 05:59 - 1998 07 09 17:5926.0118.0-26.0059.0-52.0[h]43 86 129 1720[h]42 84 126 168Cross Track Error [cm] 1998 07 02 05:59 - 1998 07 09 17:5938.0Cross Track Std. Dev. [cm] 1998 07 02 05:59 - 1998 07 09 17:5919.0100.0-19.0050.0-38.0[h]43 86 129 1720[h]42 84 126 168Figure 6-22 Tracking Accuracy of IGSO on a Loop with Custom Global NetworkR. Wolf Page 117

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