Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) for Spacecraft Attitude Tracking

Yulin Wang; Shengjing Tang; Jie Guo; Xiao Wang; Chao Liu

doi:10.1109/TAES.2019.2896873

Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) for Spacecraft Attitude Tracking

Yulin Wang, Shengjing Tang^*, Jie Guo, Xiao Wang, Chao Liu

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

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

28 Citations (Scopus)

Abstract

This paper addresses the fuzzy-logic-based fixed-time geometric backstepping attitude tracking for the rigid-body spacecraft modeled on the nonlinear differential manifold three-dimensional special orthogonal group [SO(3)]. The fixed-time geometric controller is deduced by the backstepping method. Moreover, an adaptive fuzzy logic system is employed to compensate the unknown disturbances. The almost globally fixed-time stabilization of the closed-loop system is verified via Lyapunov analysis. Simulation results demonstrate the effectiveness of the proposed controller.

Original language	English
Article number	8633933
Pages (from-to)	2938-2950
Number of pages	13
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	55
Issue number	6
DOIs	https://doi.org/10.1109/TAES.2019.2896873
Publication status	Published - Dec 2019

Keywords

Backstepping
fixed-time stabilization
fuzzy logic system (FLS)
geometric attitude control
three-dimensional special orthogonal group [SO(3)]

Access to Document

10.1109/TAES.2019.2896873

Cite this

@article{9ad46f15c9a2481cbca16e98b75a9432,

title = "Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) for Spacecraft Attitude Tracking",

abstract = "This paper addresses the fuzzy-logic-based fixed-time geometric backstepping attitude tracking for the rigid-body spacecraft modeled on the nonlinear differential manifold three-dimensional special orthogonal group [SO(3)]. The fixed-time geometric controller is deduced by the backstepping method. Moreover, an adaptive fuzzy logic system is employed to compensate the unknown disturbances. The almost globally fixed-time stabilization of the closed-loop system is verified via Lyapunov analysis. Simulation results demonstrate the effectiveness of the proposed controller.",

keywords = "Backstepping, fixed-time stabilization, fuzzy logic system (FLS), geometric attitude control, three-dimensional special orthogonal group [SO(3)]",

author = "Yulin Wang and Shengjing Tang and Jie Guo and Xiao Wang and Chao Liu",

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

year = "2019",

month = dec,

doi = "10.1109/TAES.2019.2896873",

language = "English",

volume = "55",

pages = "2938--2950",

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

issn = "0018-9251",

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

number = "6",

}

TY - JOUR

T1 - Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) for Spacecraft Attitude Tracking

AU - Wang, Yulin

AU - Tang, Shengjing

AU - Guo, Jie

AU - Wang, Xiao

AU - Liu, Chao

PY - 2019/12

Y1 - 2019/12

N2 - This paper addresses the fuzzy-logic-based fixed-time geometric backstepping attitude tracking for the rigid-body spacecraft modeled on the nonlinear differential manifold three-dimensional special orthogonal group [SO(3)]. The fixed-time geometric controller is deduced by the backstepping method. Moreover, an adaptive fuzzy logic system is employed to compensate the unknown disturbances. The almost globally fixed-time stabilization of the closed-loop system is verified via Lyapunov analysis. Simulation results demonstrate the effectiveness of the proposed controller.

AB - This paper addresses the fuzzy-logic-based fixed-time geometric backstepping attitude tracking for the rigid-body spacecraft modeled on the nonlinear differential manifold three-dimensional special orthogonal group [SO(3)]. The fixed-time geometric controller is deduced by the backstepping method. Moreover, an adaptive fuzzy logic system is employed to compensate the unknown disturbances. The almost globally fixed-time stabilization of the closed-loop system is verified via Lyapunov analysis. Simulation results demonstrate the effectiveness of the proposed controller.

KW - Backstepping

KW - fixed-time stabilization

KW - fuzzy logic system (FLS)

KW - geometric attitude control

KW - three-dimensional special orthogonal group [SO(3)]

UR - http://www.scopus.com/inward/record.url?scp=85077749302&partnerID=8YFLogxK

U2 - 10.1109/TAES.2019.2896873

DO - 10.1109/TAES.2019.2896873

M3 - Article

AN - SCOPUS:85077749302

SN - 0018-9251

VL - 55

SP - 2938

EP - 2950

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 6

M1 - 8633933

ER -

Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) for Spacecraft Attitude Tracking

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this