Distributed Robust Attitude Tracking of Multiple Spacecraft with Disturbances and Unmodelled Dynamics

Table 1

Spacecraft inertias.

Number	Parameters/(kg⋅m^2)
	1.1 0.35 0.45; 0.35 1.0 0.5; 0.45 0.5 1.3
	1 0.1 0.1; 0.1 0.1 0.1; 0.1 0.1 0.9
	1.5 0.2 0.3; 0.2 0.9 0.4; 0.3 0.4 2.0
	0.8 0.1 0.2; 0.1 0.7 0.3; 0.2 0.3 1.1
	1.2 0.3 0.7; 0.3 0.9 0.2; 0.7 0.2 1.4