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

32 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)]

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10.1109/TAES.2019.2896873

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Wang, Y., Tang, S., Guo, J., Wang, X., & Liu, C. (2019). Fuzzy-Logic-Based Fixed-Time Geometric Backstepping Control on SO(3) for Spacecraft Attitude Tracking. IEEE Transactions on Aerospace and Electronic Systems, 55(6), 2938-2950. Article 8633933. https://doi.org/10.1109/TAES.2019.2896873

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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)]",

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AU - Wang, Xiao

AU - Liu, Chao

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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.

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

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Keywords

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