Abstract
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 inter-event 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.
Funding Information
  • National Natural Science Foundation of China (62203142, 62403163)
  • China Postdoctoral Science Foundation (2022M710966, 2022TQ0096)
  • New Era-Longjiang Excellent Master
  • Ph.D Thesis Funding Project (LJYXL2022-008)
  • Aeronautical Science Foundation of China (2022Z071077009)

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