Data-driven flutter suppression of noised airfoil models: model identification and robust sliding mode control designed with multi-level control surfaces

The robust control of complex systems poses a persistent challenge in modern control theory. While several model-free robust control strategies have been developed, they often falter in the face of large perturbations. To address this issue, this paper introduces an integrated approach that combines...

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Veröffentlicht in:Nonlinear dynamics 2025-03, Vol.113 (5), p.4235-4252
Hauptverfasser: Mao, Yicheng, Liu, Xianbin
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description The robust control of complex systems poses a persistent challenge in modern control theory. While several model-free robust control strategies have been developed, they often falter in the face of large perturbations. To address this issue, this paper introduces an integrated approach that combines data-driven model identification with robust control law design paradigm. The resulting control law demonstrates robustness against both large noise perturbations and model identification errors. Furthermore, it offers advantages such as strong interference resistance, smaller control energy requirement, and enhanced stability of controlled states when compared to traditional PID control strategies. Notably, our method yields valuable insights for tackling complex control issues in general multi-degree-of-freedom Lagrangian mechanical systems, particularly those characterized by uncertain governing equations and large discontinuous perturbations.
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subjects Aircraft
Applications of Nonlinear Dynamics and Chaos Theory
Classical Mechanics
Complex systems
Control
Control algorithms
Control stability
Control surfaces
Control systems
Control theory
Degrees of freedom
Design
Dynamical Systems
Flow velocity
Identification
Mechanical systems
Noise control
Perturbation
Physics
Physics and Astronomy
Proportional integral derivative
Robust control
Sliding mode control
Statistical Physics and Dynamical Systems
Vibration
title Data-driven flutter suppression of noised airfoil models: model identification and robust sliding mode control designed with multi-level control surfaces
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