Implementation of a Differential Geometric Filter for Spacecraft Formation Orbit Estimation

Table 3

Measurement noise's set configuration.

	Minimum	Maximum	Increment
Relative Distance, (km)	0.001	0.04	0.004
Relative azimuth and elevation, (deg)	0.001	0.04	0.004
Absolute range, (km)	0.1	4	0.4
Absolute azimuth and elevation, (deg)	0.001	0.4	0.004