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