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

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

Research output: Contribution to journalArticlepeer-review

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.

Original languageEnglish
Article number110210
JournalAerospace Science and Technology
Volume163
Early online date6 May 2025
DOIs
Publication statusE-pub ahead of print - 6 May 2025

Data Availability Statement

Data will be available on reasonable request.

Funding

This work was supported in part by the University of Bristol PhD Scholarship, UK Research and Innovation (UKRI) Advanced Machinery & Productivity Initiative (AMPI) (ref: 84646), Engineering and Physical Sciences Research Council (EPSRC) RAIN+ Research Hub (EP/W001128/1), and Innovate UK Advanced Propulsion Centre (APC) ADAPT-IPT (ref: 113127). The authors would like to thank General Engine Management Systems (GEMS) Ltd. for their technical support related to the EM80-M ECU hardware implementation. The authors would like to thank the team of the ADAPT-IPT project at the Institute for Advanced Automotive Propulsion Systems (IAAPS) of the University of Bath for providing their facilities and knowledge. Thanks also go to Jon Mansfield, Mike Skinner, and Oscar Frith-Macdonald of General Engine Management Systems Ltd (GEMS) UK for their technical support on building the EM80-M coprocessor firmware.

FundersFunder number
Engineering and Physical Sciences Research Council

Keywords

  • Aero-engine
  • Air-fuel ratio
  • Emission control
  • Nonlinear dual estimators

ASJC Scopus subject areas

  • Aerospace Engineering

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