Research Article
Event-Triggered Adaptive Sliding Mode Attitude Containment Control for Microsatellite Cluster under Directed Graph
Figure 6
Simulation results of controller (19) and Figure 5. (a) Attitude of follower satellites. (b) Attitude angular velocity of follower satellites. (c) Interevent time of follower satellites 1–4. (d) Interevent time of follower satellites 5–9. (e) Control torques acting on followers. (f) Attitude trajectory of followers projected on σx-σy axis. (g) Attitude trajectory of followers on σx-σz axis. (h) Attitude trajectory of followers on σy-σz axis. (i) Triggering condition of follower satellites 1–3 within 200 s. (j) Triggering condition of follower satellites 4–6 within 200 s.
| (a) |
| (b) |
| (c) |
| (d) |
| (e) |
| (f) |
| (g) |
| (h) |
| (i) |
| (j) |