Neuro-Adaptive Fault-Tolerant Attitude Control of a Quadrotor UAV With Flight Envelope Limitation and Feedforward Compensation

To address the challenges posed by flight envelope limitation, external disturbances, model uncertainties and actuator failures in quadrotor unmanned aerial vehicles (UAVs), we propose an adaptive neural attitude control method that incorporates a Nussbaum function and nonlinear disturbance observer (NDO). By designing the Nussbaum function, we effectively address potential actuator failures while leveraging the NDO enables us to employ feedforward compensation strategy to mitigate perturbation effects. To handle the flight envelope limitation and model uncertainties, we introduce a nonlinear state-dependent function (NSDF) and neural networks (NNs), respectively. The NSDF is utilized to directly constrain the attitude, while the NNs are constructed to estimate the unknown components. Simulation results demonstrate that this approach successfully addresses the flight envelope limitation and maintains robust tracking performance even in the presence of external disturbances, model uncertainties and actuator failures in the controlled system.

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Publication Details

Journal
IEEE Transactions on Systems Man and Cybernetics Systems
Published
2025-02-26
DOI
https://doi.org/10.1109/tsmc.2025.3534986
Citations
5
Primary Topic
Adaptive Control of Nonlinear Systems
Type
article
Field-Weighted Citation Impact
6.07

Funders

Controls
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article

Neuro-Adaptive Fault-Tolerant Attitude Control of a Quadrotor UAV With Flight Envelope Limitation and Feedforward Compensation

Dengxiu Yu, Benke Gao, Lei Liu, Yan‐Jun Liu et al.
5 citations
IEEE Transactions on Systems Man and Cybernetics Systems
Adaptive Control of Nonlinear Systems
6.07
article

Neuro-Adaptive Fault-Tolerant Attitude Control of a Quadrotor UAV With Flight Envelope Limitation and Feedforward Compensation

Dengxiu Yu, Benke Gao, Lei Liu, Yan‐Jun Liu, Dapeng Li
article en
5 citations

Abstract

To address the challenges posed by flight envelope limitation, external disturbances, model uncertainties and actuator failures in quadrotor unmanned aerial vehicles (UAVs), we propose an adaptive neural attitude control method that incorporates a Nussbaum function and nonlinear disturbance observer (NDO). By designing the Nussbaum function, we effectively address potential actuator failures while leveraging the NDO enables us to employ feedforward compensation strategy to mitigate perturbation effects. To handle the flight envelope limitation and model uncertainties, we introduce a nonlinear state-dependent function (NSDF) and neural networks (NNs), respectively. The NSDF is utilized to directly constrain the attitude, while the NNs are constructed to estimate the unknown components. Simulation results demonstrate that this approach successfully addresses the flight envelope limitation and maintains robust tracking performance even in the presence of external disturbances, model uncertainties and actuator failures in the controlled system.

IEEE Transactions on Systems Man and Cybernetics SystemsVol. 55(5)
Northwestern Polytechnical University (CN), Liaoning University of Technology (CN)
National Natural Science Foundation of China, Liaoning Revitalization Talents Program
Affordable and clean energy
Openalex Percentile: Top 4%
Adaptive Control of Nonlinear Systems
6.07
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