Cascade-Based Controlled Attitude Synchronization and Tracking of Spacecraft in Leader-Follower Formation

Figure 2

Attitude and angular velocity error and control torque for leader ((a), (c), (e)) and synchronizing follower ((b), (d), (f)) spacecraft during maneuver without measurement noise and disturbances.

(a)

(b)

(c)

(d)

(e)

(f)