Abstract
This brief investigates event-triggered control for spacecraft attitude stabilization under the influence of actuator output nonlinearities. Under a designed event-triggered policy, the influences of actuators' inherent nonlinearity and network quantized transmission are evaluated under a unified framework. Compared with the previous results, the influences of data transmission and actuators' inherent nonlinearities are uniformly described as the actuator output nonlinearities, and the event-triggered policy reduces the effects of constants commonly introduced into triggering conditions on the final state convergence regions and achieves Zeno-free triggering. Simulations verify theoretical results.
| Original language | English |
|---|---|
| Article number | 9345979 |
| Pages (from-to) | 2855-2859 |
| Number of pages | 5 |
| Journal | IEEE Transactions on Circuits and Systems II: Express Briefs |
| Volume | 68 |
| Issue number | 8 |
| DOIs | |
| State | Published - Aug 2021 |
Keywords
- actuator output nonlinearities
- event-triggered sampling
- Spacecraft attitude control