Event-triggered fault tolerant control for spacecraft formation attitude synchronization with limited data communication. (English) Zbl 1415.93241
Summary: This paper investigates the leader-following attitude consensus problem of a group of \(n\)-th spacecrafts with actuator fault and limited data communication, where the event-triggered based sending mechanism is considered to decrease communication burthen. In this design, unknown actuator faults and external disturbances are considered, and an event-triggered based adaptive distributed cooperative attitude control law is developed to solve the multiple spacecrafts formation control problem. It is shown that leader-following attitude synchronization can be achieved under the designed event-triggered control law. Finally, a simulation example is provided to illustrate the effectiveness of the proposed attitude coordination control techniques.
MSC:
| 93D99 | Stability of control systems |
| 93C95 | Application models in control theory |
| 93A13 | Hierarchical systems |
| 93C65 | Discrete event control/observation systems |
| 93B12 | Variable structure systems |
Keywords:
spacecraft formation attitude consensus; actuator faults; sliding mode control; event-triggered controlReferences:
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