T-S Fuzzy-Based Event-Triggering Attitude-Tracking Control for Elastic Spacecraft with Quantization

Ang Li; Choon Ki Ahn; Ming Liu

doi:10.1109/TAES.2021.3097952

T-S Fuzzy-Based Event-Triggering Attitude-Tracking Control for Elastic Spacecraft with Quantization

Ang Li, Choon Ki Ahn, Ming Liu

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

4 Citations (Scopus)

Abstract

Based on the T-S fuzzy modeling method, this article aims to deal with the problem of event-triggered integral sliding-mode attitude-tracking control for a nonlinear elastic spacecraft system with the unknown actuator dead-zone and a redundant reaction wheel over digital communication channels. Considering the effect of external disturbance and the restrictions imposed by wireless network transmission, a classical dynamic logarithmic sensor-to-controller quantizer and an event-triggered mechanism are introduced to perform the analysis and design work. The T-S fuzzy model is introduced to describe the nonlinear attitude dynamic property of the flexible spacecraft, and an integral sliding surface is employed in this article. The robustness of the closed-loop attitude-tracking control system and the finite-time reachability of the sliding-surface domain are guaranteed by the presented quantized event-triggering adaptive sliding-mode control law. Simulation results are provided to verify the feasibility of the proposed attitude-tracking control strategy.

Original language	English
Pages (from-to)	124-139
Number of pages	16
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	58
Issue number	1
DOIs	https://doi.org/10.1109/TAES.2021.3097952
Publication status	Published - 2022 Feb 1

Keywords

Digital communication channel
Elastic spacecraft attitude tracking
Event-triggered control
Integral sliding-mode control
T-S fuzzy model

ASJC Scopus subject areas

Aerospace Engineering
Electrical and Electronic Engineering

Access to Document

10.1109/TAES.2021.3097952

Cite this

@article{ce6462b144614fed9a752088efc2d9df,

title = "T-S Fuzzy-Based Event-Triggering Attitude-Tracking Control for Elastic Spacecraft with Quantization",

abstract = "Based on the T-S fuzzy modeling method, this article aims to deal with the problem of event-triggered integral sliding-mode attitude-tracking control for a nonlinear elastic spacecraft system with the unknown actuator dead-zone and a redundant reaction wheel over digital communication channels. Considering the effect of external disturbance and the restrictions imposed by wireless network transmission, a classical dynamic logarithmic sensor-to-controller quantizer and an event-triggered mechanism are introduced to perform the analysis and design work. The T-S fuzzy model is introduced to describe the nonlinear attitude dynamic property of the flexible spacecraft, and an integral sliding surface is employed in this article. The robustness of the closed-loop attitude-tracking control system and the finite-time reachability of the sliding-surface domain are guaranteed by the presented quantized event-triggering adaptive sliding-mode control law. Simulation results are provided to verify the feasibility of the proposed attitude-tracking control strategy. ",

keywords = "Digital communication channel, Elastic spacecraft attitude tracking, Event-triggered control, Integral sliding-mode control, T-S fuzzy model",

author = "Ang Li and Ahn, {Choon Ki} and Ming Liu",

note = "Funding Information: This work was supported in part by the Chinese Scholarship Council under Grant 201906120101, in part by the National Natural Science Foundation of China under Grant 61833009 and Grant 61690212, and in part by the National Research Foundation of Korea (NRF) grant Funded by the Korea Government (Ministry of Science and ICT) under Grant NRF-2020R1A2C1005449. Publisher Copyright: {\textcopyright} 1965-2011 IEEE.",

year = "2022",

month = feb,

day = "1",

doi = "10.1109/TAES.2021.3097952",

language = "English",

volume = "58",

pages = "124--139",

journal = "IEEE Transactions on Aerospace and Electronic Systems",

issn = "0018-9251",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

number = "1",

}

TY - JOUR

T1 - T-S Fuzzy-Based Event-Triggering Attitude-Tracking Control for Elastic Spacecraft with Quantization

AU - Li, Ang

AU - Ahn, Choon Ki

AU - Liu, Ming

N1 - Funding Information: This work was supported in part by the Chinese Scholarship Council under Grant 201906120101, in part by the National Natural Science Foundation of China under Grant 61833009 and Grant 61690212, and in part by the National Research Foundation of Korea (NRF) grant Funded by the Korea Government (Ministry of Science and ICT) under Grant NRF-2020R1A2C1005449. Publisher Copyright: © 1965-2011 IEEE.

PY - 2022/2/1

Y1 - 2022/2/1

N2 - Based on the T-S fuzzy modeling method, this article aims to deal with the problem of event-triggered integral sliding-mode attitude-tracking control for a nonlinear elastic spacecraft system with the unknown actuator dead-zone and a redundant reaction wheel over digital communication channels. Considering the effect of external disturbance and the restrictions imposed by wireless network transmission, a classical dynamic logarithmic sensor-to-controller quantizer and an event-triggered mechanism are introduced to perform the analysis and design work. The T-S fuzzy model is introduced to describe the nonlinear attitude dynamic property of the flexible spacecraft, and an integral sliding surface is employed in this article. The robustness of the closed-loop attitude-tracking control system and the finite-time reachability of the sliding-surface domain are guaranteed by the presented quantized event-triggering adaptive sliding-mode control law. Simulation results are provided to verify the feasibility of the proposed attitude-tracking control strategy.

AB - Based on the T-S fuzzy modeling method, this article aims to deal with the problem of event-triggered integral sliding-mode attitude-tracking control for a nonlinear elastic spacecraft system with the unknown actuator dead-zone and a redundant reaction wheel over digital communication channels. Considering the effect of external disturbance and the restrictions imposed by wireless network transmission, a classical dynamic logarithmic sensor-to-controller quantizer and an event-triggered mechanism are introduced to perform the analysis and design work. The T-S fuzzy model is introduced to describe the nonlinear attitude dynamic property of the flexible spacecraft, and an integral sliding surface is employed in this article. The robustness of the closed-loop attitude-tracking control system and the finite-time reachability of the sliding-surface domain are guaranteed by the presented quantized event-triggering adaptive sliding-mode control law. Simulation results are provided to verify the feasibility of the proposed attitude-tracking control strategy.

KW - Digital communication channel

KW - Elastic spacecraft attitude tracking

KW - Event-triggered control

KW - Integral sliding-mode control

KW - T-S fuzzy model

UR - http://www.scopus.com/inward/record.url?scp=85111556020&partnerID=8YFLogxK

U2 - 10.1109/TAES.2021.3097952

DO - 10.1109/TAES.2021.3097952

M3 - Article

AN - SCOPUS:85111556020

SN - 0018-9251

VL - 58

SP - 124

EP - 139

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 1

ER -

T-S Fuzzy-Based Event-Triggering Attitude-Tracking Control for Elastic Spacecraft with Quantization

Abstract

Keywords

ASJC Scopus subject areas

Access to Document

Other files and links

Fingerprint

Cite this