https://orcid.org/0000-0001-7902-0570
https://orcid.org/0000-0002-1464-6721
https://orcid.org/0000-0002-8789-6246
https://orcid.org/0000-0003-1329-4442
https://orcid.org/0000-0003-0474-953X
https://orcid.org/0000-0001-7902-0570
https://orcid.org/0000-0002-1464-6721
https://orcid.org/0000-0002-8789-6246
https://orcid.org/0000-0003-1329-4442
https://orcid.org/0000-0003-0474-953X
The article proposes a dynamic time-varying event-triggered strategy to achieve semi-global finite-time rendezvous control of saturated spacecraft. The main idea of the designed dynamic event-triggered strategy is to construct the controller that contains the time-varying high-gain and a dynamic event-triggered mechanism simultaneously. Moreover, a positive lower bound of interevent times is obtained by using the properties of the parametric Lyapunov equation, such that the Zeno phenomenon is eliminated. Finally, the designed dynamic time-varying event-triggered strategy is verified by simulation results.
Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy
IEEE Transactions on Aerospace and Electronic Systems ; 61 , 2 ; 5395-5401
2025-04-01
792582 byte
Article (Journal)
Electronic Resource
English
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