Research Article
Estimation and Analysis of Powered Phase’s Orbit of the Spacecraft Based on Multiple-Point Intersection Algorithm
Table 1
The three-dimensional position of observation satellite 02 at the sampling point.
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| | 50.0 | 1.773806e + 06 | 8.161384e + 06 | 4.516700e + 06 | | 100.0 | 1.501626e + 06 | 8.126764e + 06 | 4.684680e + 06 | | 150.0 | 1.227700e + 06 | 8.082699e + 06 | 4.847216e + 06 | | 200.0 | 9.523491e + 05 | 8.029253e + 06 | 5.004127e + 06 | | 250.0 | 6.956792e + 05 | 7.971293e + 06 | 5.144636e + 06 |
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