Cooperative Attitude Control of Multiple Rigid Bodies with Multiple Time-Varying Delays and Dynamically Changing Topologies

Table 1

Spacecraft specifications.

$J_1$	[$2$3.0 0.1 0.1; 0.1 22.2 0.1; 0.1 0.1 23.2] $\text{kg}·{\text{m}}^2$
$J_2$	[$2$2.5 0.1 $-0.3$; 0.1 22.1 0.1; $-0.3$ 0.1 24.1] $\text{kg}·{\text{m}}^2$
$J_3$	[24.0 $-0.2$ 0.1; 0 21.2 0.1; 0.1 $-0.1$ 22.2] $\text{kg}·{\text{m}}^2$