Adaptive Fault-Tolerant Control for Attitude Tracking of a Carrier-Based Aircraft Subject to Actuator Faults

This article presents a fault-tolerant attitude tracking control for carrier-based aircraft subject to actuator faults. The proposed controller adopts nonlinear dynamic inversion (NDI) to ensure asymptotic attitude tracking for the fault-free attitude system and employs <inline-formula><tex...

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Published inIEEE transactions on aerospace and electronic systems Vol. 60; no. 5; pp. 6133 - 6145
Main Authors Liu, Simin, Zheng, Zewei, Zhu, Bing, Guan, Zhiyuan
Format Journal Article
LanguageEnglish
Published New York IEEE 01.10.2024
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects
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Actuators
Adaptation models
Adaptive control
Adaptive sampling
Adaptive systems
Aircraft
Aircraft control
Attitude control
carrier-based aircraft
Closed loops
Data acquisition
Dynamic inversion
Dynamical systems
Fault tolerance
Fault tolerant systems
fault-tolerant control
Faults
Nonlinear control
Nonlinear dynamics
Reference systems
Tracking control
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ISSN0018-9251
1557-9603
DOI10.1109/TAES.2024.3401672

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Abstract This article presents a fault-tolerant attitude tracking control for carrier-based aircraft subject to actuator faults. The proposed controller adopts nonlinear dynamic inversion (NDI) to ensure asymptotic attitude tracking for the fault-free attitude system and employs <inline-formula><tex-math notation="LaTeX">\mathcal{L}_{1}</tex-math></inline-formula> piecewise constant adaptive law to compensate for errors caused by actuator lock-in-place (LIP) faults. Theoretical analysis indicates that by reducing the sampling time of the adaptive law, the performance difference bounds of the closed-loop <inline-formula><tex-math notation="LaTeX">\mathcal{L}_{1}</tex-math></inline-formula> adaptive system and the closed-loop reference system can be adjusted to be arbitrarily small. The fault-tolerant performance of the proposed method is supported by data acquired from flight tests.
AbstractList This article presents a fault-tolerant attitude tracking control for carrier-based aircraft subject to actuator faults. The proposed controller adopts nonlinear dynamic inversion (NDI) to ensure asymptotic attitude tracking for the fault-free attitude system and employs <inline-formula><tex-math notation="LaTeX">\mathcal{L}_{1}</tex-math></inline-formula> piecewise constant adaptive law to compensate for errors caused by actuator lock-in-place (LIP) faults. Theoretical analysis indicates that by reducing the sampling time of the adaptive law, the performance difference bounds of the closed-loop <inline-formula><tex-math notation="LaTeX">\mathcal{L}_{1}</tex-math></inline-formula> adaptive system and the closed-loop reference system can be adjusted to be arbitrarily small. The fault-tolerant performance of the proposed method is supported by data acquired from flight tests.
This article presents a fault-tolerant attitude tracking control for carrier-based aircraft subject to actuator faults. The proposed controller adopts nonlinear dynamic inversion (NDI) to ensure asymptotic attitude tracking for the fault-free attitude system and employs [Formula Omitted] piecewise constant adaptive law to compensate for errors caused by actuator lock-in-place (LIP) faults. Theoretical analysis indicates that by reducing the sampling time of the adaptive law, the performance difference bounds of the closed-loop [Formula Omitted] adaptive system and the closed-loop reference system can be adjusted to be arbitrarily small. The fault-tolerant performance of the proposed method is supported by data acquired from flight tests.
Author Liu, Simin
Zhu, Bing
Guan, Zhiyuan
Zheng, Zewei
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Actuators
Adaptation models
Adaptive control
Adaptive sampling
Adaptive systems
Aircraft
Aircraft control
Attitude control
carrier-based aircraft
Closed loops
Data acquisition
Dynamic inversion
Dynamical systems
Fault tolerance
Fault tolerant systems
fault-tolerant control
Faults
Nonlinear control
Nonlinear dynamics
Reference systems
Tracking control
Title Adaptive Fault-Tolerant Control for Attitude Tracking of a Carrier-Based Aircraft Subject to Actuator Faults
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