Model Predictive and Reinforcement Learning Methods for Active Flow Control of an Airfoil with Dual-point Excitation of Plasma Actuators
AmirHossein Ghaemi, Abbas Ebrahimi, Majid Hajipour, Seyyed Mohammad Mahdy Shobeiry, Arash Fath Lipaei

TL;DR
This paper compares Model Predictive Control and Reinforcement Learning techniques for active flow control over an airfoil, demonstrating RL's faster adaptation and comparable effectiveness in flow separation management.
Contribution
It introduces a novel comparison between RL and MPC for plasma actuator-based flow control, highlighting RL's rapid adaptation capabilities in real-time aerodynamic applications.
Findings
RL optimized excitation frequency achieving Cl=1.62 in under 2.5 seconds.
Adaptive MPC achieved Cl=1.60 at 110 Hz but struggled near physical limits.
RL methods outperform MPC in dynamic, real-time flow control scenarios.
Abstract
This study investigates the effectiveness of Model Predictive Control (MPC) and Reinforcement Learning (RL) for active flow control over a NACA 4412 airfoil near static stall at Reynolds number 4*10^5. By systematically evaluating these strategies, the research addresses a critical gap in optimizing excitation frequency and improving response time in flow control. The work contributes to understanding RL adaptability and performance versus MPC in aerodynamic flow separation control. Numerical simulations of the Reynolds Averaged Navier-Stokes equations with the Scale-Adaptive Simulation turbulence model are used. Dielectric Barrier Discharge plasma actuators in dual-point excitation mode control flow separation. The study evaluates adaptive MPC, temporal difference RL (TDRL), and deep Q-learning (DQL) for optimizing excitation frequency and expediting stabilization. An integrated signal…
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Taxonomy
TopicsPlasma and Flow Control in Aerodynamics · Fluid Dynamics and Turbulent Flows · Computational Fluid Dynamics and Aerodynamics
