Active control of road vehicle’s drag for varying upstream flow conditions using a recursive subspace based predictive control methodology

The growing focus on reducing energy consumption, particularly in electric vehicles with limited autonomy, has prompted innovative solutions. In this context, we propose a real-time flap-based control system aimed at improving aerodynamic drag in real driving conditions. Employing a Recursive Subspace based Predictive Control approach, we conducted wind tunnel tests on a representative model vehicle at reduced scale equipped with flaps. Comprehensive assessments using pressure measurements and Particle Image Velocimetry were undertaken to evaluate the control efficiency. Static and dynamic perturbation tests were conducted, revealing the system’s effectiveness in both scenarios. The closed-loop controlled system demonstrated a substantial gain, achieving a 5% base pressure recovery.

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Publication Details

Journal
Control Engineering Practice
Published
2024-08-31
DOI
https://doi.org/10.1016/j.conengprac.2024.106071
Citations
4
Primary Topic
Aerodynamics and Fluid Dynamics Research
Type
article
Field-Weighted Citation Impact
5.20
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Active control of road vehicle’s drag for varying upstream flow conditions using a recursive subspace based predictive control methodology

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article

Active control of road vehicle’s drag for varying upstream flow conditions using a recursive subspace based predictive control methodology

Jacques Borée, Guillaume Mercère, Patrick Coirault, Clément Dumand, Agostino Cembalo
article en
4 citations

Abstract

The growing focus on reducing energy consumption, particularly in electric vehicles with limited autonomy, has prompted innovative solutions. In this context, we propose a real-time flap-based control system aimed at improving aerodynamic drag in real driving conditions. Employing a Recursive Subspace based Predictive Control approach, we conducted wind tunnel tests on a representative model vehicle at reduced scale equipped with flaps. Comprehensive assessments using pressure measurements and Particle Image Velocimetry were undertaken to evaluate the control efficiency. Static and dynamic perturbation tests were conducted, revealing the system’s effectiveness in both scenarios. The closed-loop controlled system demonstrated a substantial gain, achieving a 5% base pressure recovery.

Control Engineering PracticeVol. 152
Centre National de la Recherche Scientifique (FR), École Nationale Supérieure de Mécanique et d'Aérotechnique (FR), Institut Pprime (FR), Université de Poitiers (FR), Laboratoire d'Informatique et d'Automatique pour les Systèmes (FR), Carrier (United States) (US)
Climate action
Openalex Percentile: Top 5%
Aerodynamics and Fluid Dynamics Research
5.20
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