Implementation of a Differential Geometric Filter for Spacecraft Formation Orbit Estimation

Table 1

Spacecraft formation's configuration for short, medium, and long range formation.

	Short				Medium				Long
	S/C 1	S/C 2	S/C 3	S/C 4	S/C 1	S/C 2	S/C 3	S/C 4	S/C 1	S/C 2	S/C 3	S/C 4
RAAN (deg)	0	0	0	0	−0.1	0	0	0.1	0.2	0	−0.1	0.1
INC (deg)	15	15	15	15	14.5	14	15.5	15	15	20	25	10
ARGPER (deg)	0	0.001	−0.001	0.002	0.2	0	−0.1	0.1	0	5	−5	10