Closed-loop supersonic flow control with a high-speed experimental deep reinforcement learning framework
Although active flow control based on deep reinforcement learning (DRL) has been demonstrated extensively in numerical environments, practical implementation of real-time DRL control in experiments remains challenging, largely because of the critical time requirement imposed on data acquisition and neural-network computation. In this study, a high-speed field-programmable gate array (FPGA) -based experimental DRL (FeDRL) control framework is developed, capable of achieving a control frequency of 1–10 kHz, two orders higher than that of the existing CPU-based framework (10 Hz). The feasibility of the FeDRL framework is tested in a rather challenging case of supersonic backward-facing step flow at Mach 2, with an array of plasma synthetic jets and a hot-wire acting as the actuator and sensor, respectively. The closed-loop control law is represented by a radial basis function network and optimised by a classical value-based algorithm (i.e. deep Q-network). Results show that, with only ten seconds of training, the agent is able to find a satisfying control law that increases the mixing in the shear layer by 21.2 %. Such a high training efficiency has never been reported in previous experiments (typical time cost: hours).
Authors
- Haohua Zong (ORCID: https://orcid.org/0000-0002-9037-0528)
- Zhi Su (ORCID: https://orcid.org/0000-0002-0604-9214)
- Hua Liang (ORCID: https://orcid.org/0000-0003-2547-2701)
- Jinping Li
- Yun Wu
Institutions
- Air Force Engineering University (CN)
- Xi'an Jiaotong University (CN)
Publication Details
- Journal
- Journal of Fluid Mechanics
- Published
- 2025-04-11
- DOI
- https://doi.org/10.1017/jfm.2025.160
- Citations
- 36
- Primary Topic
- Plasma and Flow Control in Aerodynamics
- Type
- article
- Field-Weighted Citation Impact
- 179.77
Funders
- National Natural Science Foundation of China