Event-Triggered Adaptive Sliding Mode Attitude Containment Control for Microsatellite Cluster under Directed Graph

Figure 3

Simulation results of controller (19) and Figure 2. (a) Attitude of follower satellites. (b) Attitude angular velocity of follower satellites. (c) Interevent time of follower satellites 1–3. (d) Interevent time of follower satellites 4–6. (e) Control torques acting on followers. (f) Attitude trajectories of follower satellites. (g) Triggering condition of follower satellites 1–3 in 200 s. (h) Triggering condition of follower satellites 4–6 in 200 s.

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