Reinforcement Learning–Based Adaptive Fault-Tolerant Antidisturbance Control for UAVs Subjected to External Disturbances, Input Uncertainties, and Structural Uncertainties

This paper presents a reinforcement learning (RL)–based adaptive fault-tolerant control scheme for quadrotor unmanned aerial vehicles (UAVs) subjected to external disturbances, input uncertainties, and structural uncertainties. In practical engineering, UAV systems often are influenced by aforementioned multiple-source coupled uncertainties, making it challenging to design effective controllers. Herein, first, by introducing a penalty function, a critic network is established to evaluate control performance. Subsequently, the output signals of the critic network are introduced into the updating of actor network, functioning as a reinforcement signal to drive the actor network to approximate unknown nonlinearities. Moreover, an adaptive disturbance boundary estimator is constructed to attenuate the external disturbances and network errors, which are defined collectively in a lumped disturbance set. Additionally, a series of adaptive compensating laws are developed to deal with the input uncertainties. Finally, to tackle multisource coupled uncertainties, a novel RL-based adaptive fault-tolerant controller is proposed which integrates the RL framework, adaptive disturbance boundary estimator, and adaptive input uncertainty compensating laws. Analyzing the Lyapunov function proved that the controlled system is asymptotically stable and all signals are bounded. Numerical simulations revealed the effectiveness and superiority of the proposed method.

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Publication Details

Journal
Journal of Aerospace Engineering
Published
2024-09-30
DOI
https://doi.org/10.1061/jaeeez.aseng-5655
Citations
3
Primary Topic
Adaptive Dynamic Programming Control
Type
article
Field-Weighted Citation Impact
1.08
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article

Reinforcement Learning–Based Adaptive Fault-Tolerant Antidisturbance Control for UAVs Subjected to External Disturbances, Input Uncertainties, and Structural Uncertainties

Likuan Qiu, Yuxuan Chang, Zheng Wang, Shiyu Wang et al.
3 citations
Journal of Aerospace Engineering
Adaptive Dynamic Programming Control
1.08
article

Reinforcement Learning–Based Adaptive Fault-Tolerant Antidisturbance Control for UAVs Subjected to External Disturbances, Input Uncertainties, and Structural Uncertainties

Likuan Qiu, Yuxuan Chang, Zheng Wang, Shiyu Wang, Yunfei Bai
article en
3 citations

Abstract

This paper presents a reinforcement learning (RL)–based adaptive fault-tolerant control scheme for quadrotor unmanned aerial vehicles (UAVs) subjected to external disturbances, input uncertainties, and structural uncertainties. In practical engineering, UAV systems often are influenced by aforementioned multiple-source coupled uncertainties, making it challenging to design effective controllers. Herein, first, by introducing a penalty function, a critic network is established to evaluate control performance. Subsequently, the output signals of the critic network are introduced into the updating of actor network, functioning as a reinforcement signal to drive the actor network to approximate unknown nonlinearities. Moreover, an adaptive disturbance boundary estimator is constructed to attenuate the external disturbances and network errors, which are defined collectively in a lumped disturbance set. Additionally, a series of adaptive compensating laws are developed to deal with the input uncertainties. Finally, to tackle multisource coupled uncertainties, a novel RL-based adaptive fault-tolerant controller is proposed which integrates the RL framework, adaptive disturbance boundary estimator, and adaptive input uncertainty compensating laws. Analyzing the Lyapunov function proved that the controlled system is asymptotically stable and all signals are bounded. Numerical simulations revealed the effectiveness and superiority of the proposed method.

Journal of Aerospace EngineeringVol. 38(1)
Northwestern Polytechnical University (CN), SGIDI Engineering Consulting (China) (CN), China Academy of Launch Vehicle Technology (CN)
Climate action
Openalex Percentile: Top 20%
Adaptive Dynamic Programming Control
1.08
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