Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy

Kai Zhang; Xuefei Yang; Zhijian Hu; Meilin Li; Tieshan Li

doi:10.1109/TAES.2024.3480895

Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy

Kai Zhang
, Xuefei Yang
, Zhijian Hu^*
, Meilin Li^*
, Tieshan Li

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology
State Key Laboratory of Integrated Services Networks
Toulouse University, UPS-OMP, IRAP
Nanyang Technological University
University of Electronic Science and Technology of China

Research output: Contribution to journal › Article › peer-review

5 Scopus citations

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 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.

Original language	English
Pages (from-to)	5395-5401
Number of pages	7
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	61
Issue number	2
DOIs	https://doi.org/10.1109/TAES.2024.3480895
State	Published - 2025

Keywords

Dynamic event-triggered mechanism
finite-time control
minimal interevent time
saturated spacecraft rendezvous system
time-varying gain

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10.1109/TAES.2024.3480895

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title = "Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy",

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 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.",

keywords = "Dynamic event-triggered mechanism, finite-time control, minimal interevent time, saturated spacecraft rendezvous system, time-varying gain",

author = "Kai Zhang and Xuefei Yang and Zhijian Hu and Meilin Li and Tieshan Li",

note = "Publisher Copyright: {\textcopyright} 1965-2011 IEEE.",

year = "2025",

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T1 - Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy

AU - Zhang, Kai

AU - Yang, Xuefei

AU - Hu, Zhijian

AU - Li, Meilin

AU - Li, Tieshan

PY - 2025

Y1 - 2025

N2 - 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.

AB - 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.

KW - Dynamic event-triggered mechanism

KW - finite-time control

KW - minimal interevent time

KW - saturated spacecraft rendezvous system

KW - time-varying gain

UR - https://www.scopus.com/pages/publications/105002493594

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DO - 10.1109/TAES.2024.3480895

M3 - 文章

AN - SCOPUS:105002493594

SN - 0018-9251

VL - 61

SP - 5395

EP - 5401

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 2

ER -

Semiglobal Finite-Time Rendezvous Control of Saturated Spacecraft by Dynamic Time-Varying Event-Triggered Strategy

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Keywords

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