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

^*此作品的通讯作者

宇航学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

28 引用（Scopus）

摘要

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.

源语言	英语
文章编号	8633933
页（从-至）	2938-2950
页数	13
期刊	IEEE Transactions on Aerospace and Electronic Systems
卷	55
期	6
DOI	https://doi.org/10.1109/TAES.2019.2896873
出版状态	已出版 - 12月 2019

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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.",

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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)]

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

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