Effective emission control of aero-engines via nonlinear dual-estimators for uncertain states and parameters
This paper proposes an effective emission control strategy for an aero-engine using nonlinear dual-estimators, which aims to address challenges arising from state and parameter uncertainties. Transient air-fuel ratio (AFR) regulation issues, primarily caused by the wall-wetting and manifold-filling phenomena, are mitigated by a novel approach leveraging dual nonlinear estimators: (i) an extended Kalman filter (EKF) and (ii) an unknown dynamics estimator (UDE). The EKF estimates the fuel mass flow rate and unknown internal parameters, while the UDE compensates for nonlinear air-filling dynamics by estimating a lumped term involving the second derivative of air mass flow. The control framework is built upon a modified mean value engine model (MVEM), tailored to capture the unique dynamics of the rotary aero-engine. Building upon the foundational concepts developed in earlier research, this work moves toward practical application by demonstrating the proposed strategy through real-world experiments conducted on an AIE 225CS rotary aero-engine under a standard driving cycle, marking a significant step forward from theory to application. Furthermore, it introduces a complete stability analysis that addresses the coupling of dual-estimation errors, an aspect not explored in prior work. Comparative experimental results against an industry-standard gain-scheduling PID controller demonstrate the proposed method's performance in achieving improved AFR regulation and significant emissions reduction. • A novel dual-estimator control strategy effectively addresses AFR transient challenges. • Real-world experiments on a Wankel rotary aero-engine validate the proposed method. • The controller reduces emissions effectively by stabilizing AFR near stoichiometric levels. • Simplified implementation eliminates the need for extensive calibration and additional sensors.
Authors
- Reza Islam
- Guido Herrmann (ORCID: https://orcid.org/0000-0001-5390-4538)
- Chris Brace (ORCID: https://orcid.org/0000-0003-4594-0218)
- Nathan Bailey (ORCID: https://orcid.org/0000-0003-3480-7390)
- Stuart C Burgess (ORCID: https://orcid.org/0000-0002-2689-508X)
- Anthony Siming Chen (ORCID: https://orcid.org/0000-0001-8940-7250)
- Giovanni Vorraro (ORCID: https://orcid.org/0000-0002-1859-4287)
- James W. G. Turner (ORCID: https://orcid.org/0000-0001-6691-5770)
- Matthew Turner (ORCID: https://orcid.org/0000-0002-9051-5846)
Institutions
- University of Nottingham (GB)
- University of Manchester (GB)
- University of Bristol (GB)
- Advanced Innovative Engineering (United Kingdom) (GB)
- University of Bath (GB)
- King Abdullah University of Science and Technology (SA)
Publication Details
- Journal
- Aerospace Science and Technology
- Published
- 2025-05-06
- DOI
- https://doi.org/10.1016/j.ast.2025.110210
- Citations
- 2
- Primary Topic
- Advanced Control Systems Optimization
- Type
- article
- Field-Weighted Citation Impact
- 2.43
Funders
- UK Research and Innovation
- University of Bristol
- Engineering and Physical Sciences Research Council
- Innovate UK