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Precise Orbit Determination of Global Navigation Satellite System of ...

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Chapter 9 S<strong>of</strong>tware and Simulation Results<br />

Ambiguity<br />

101<br />

100.5<br />

100<br />

99.5<br />

99<br />

0 24 48 72 96 120 144 168 192 216 240<br />

Time (hour)<br />

Figure 9-42 Float Ambiguity Solution <strong>of</strong> an IGSO <strong>Satellite</strong> at λ=-10° at Tracking Station 5<br />

Figure 9-40 shows the accuracies <strong>of</strong> x, y, z coordinates <strong>of</strong> orbit determination <strong>of</strong> an IGSO satellite located at λ=-<br />

10° with float ambiguity solution considering the satellite visibility and observation sample rate 1 min are ±0.04<br />

m, ±0.05 m and ±0.02 m respectively. Figure 9-41 and Figure 9-42 show the related ambiguity solution.<br />

Difference (meter)<br />

1<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0<br />

-0.2<br />

-0.4<br />

-0.6<br />

-0.8<br />

-1<br />

0 24 48 72 96 120 144 168 192 216 240<br />

Time (hour)<br />

Figure 9-43 Accuracy <strong>of</strong> Dynamic <strong>Orbit</strong> <strong>Determination</strong> <strong>of</strong> an IGSO <strong>Satellite</strong> at λ=20° with Float Ambiguity Solution and<br />

Sample Rate 1 min<br />

132<br />

dx<br />

dy<br />

dz

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