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

Institutions

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

Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Effective emission control of aero-engines via nonlinear dual-estimators for uncertain states and parameters

Reza Islam, Guido Herrmann, Chris Brace, Nathan Bailey et al.
2 citations
Aerospace Science and Technology
Advanced Control Systems Optimization
2.43
article

Effective emission control of aero-engines via nonlinear dual-estimators for uncertain states and parameters

Reza Islam, Guido Herrmann, Chris Brace, Nathan Bailey, Stuart C Burgess, Anthony Siming Chen, Giovanni Vorraro, James W. G. Turner, Matthew Turner
article en
2 citations

Abstract

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.

Aerospace Science and TechnologyVol. 163
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)
UK Research and Innovation, University of Bristol, Engineering and Physical Sciences Research Council, Innovate UK
Climate action
Openalex Percentile: Top 12%
Advanced Control Systems Optimization
2.43
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.