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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>6.2.2 IGSO Walker Constellation6.2.2.1 Ground TrackingThe IGSO Walker constellation is reasonably good tracked by custom global networkproviding 3 – 4 simultaneous ground links. The st<strong>and</strong>ard deviation in radial direction isaround 35 cm.Radial Error [cm] 1998 07 02 10:09 - 1998 07 09 22:09118.0Radial Std. Dev. [cm] 1998 07 02 10:09 - 1998 07 09 22:0959.032.0-59.0016.0-118.0[h]39 78 117 1560[h]39 78 117 156Along Track Error [cm] 1998 07 02 10:09 - 1998 07 09 22:09126.0Along Track Std. Dev. [cm] 1998 07 02 10:09 - 1998 07 09 22:0963.098.0-63.0049.0-126.0[h]39 78 117 1560[h]39 78 117 156Cross T rack Error [cm] 1998 07 02 10:09 - 1998 07 09 22:09134.0Cross T rack Std. Dev. [cm] 1998 07 02 10:09 - 1998 07 09 22:0967.0120.0-67.0060.0-134.0[h]39 78 117 1560[h]39 78 117 156Figure 6-19 Tracking Accuracy with Custom Global NetPage 114R. Wolf

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