Development of a Digital Twin for Electrified Aircraft Powertrain Health Management

Thomas W Kennings; Donald L Simon

NASA NTRS · 20260004592

Development of a Digital Twin for Electrified Aircraft Powertrain Health Management

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Abstract

The augmentation of aircraft powertrains with electrical power systems is a promising path to reducing aircraft fuel consumption, emissions, and noise. Like conventional propulsion systems, electrified aircraft propulsion (EAP) systems will be subject to wear and tear throughout their lifecycles. System health management for EAP will enable efficient flight and maintenance scheduling, realizing economic, safety, and reliability benefits. A digital twin is, broadly, a dynamically updated virtual representation of an individual physical asset. This paper presents a Kalman filter-based approach for the development of a digital twin for an electrified powertrain and applies the approach to an EAP controls testbed. Measurements from nominal testbed operations are used to update a nonlinear model of the testbed. A Kalman filter is then created and used to identify and isolate anomalous testbed behavior based on measurements from off- nominal operations. Results show that the Kalman filter-based digital twin can monitor individual powertrain components’ health for degradation or other changes in performance. The applicability of the presented digital twin approach to any hybrid- or fully-electrified powertrain is emphasized.

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Electrified Aircraft Propulsion Digital Twin System Health Management Kalman Filter

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Thomas W Kennings, Donald L Simon. Development of a Digital Twin for Electrified Aircraft Powertrain Health Management. https://ntrs.nasa.gov/citations/20260004592

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