Research Article
Decentralized State Estimation Algorithm of Centralized Equivalent Precision for Formation Flying Spacecrafts Based on Junction Tree
Table 1
Keplerian orbital elements of a satellite formation.
| Sat number | (km) | | (°) | (°) | (°) | (°) |
| 1 | 8400.000000 | 0.005000 | 30.000000 | 120.000000 | 0.000000 | 90.000000 | 2 | 8400.000000 | 0.004743 | 29.996649 | 119.988151 | 1.783138 | 88.250782 | 3 | 8400.000000 | 0.004743 | 30.003353 | 120.011847 | 1.762616 | 88.250782 |
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