Abstract
This paper presents a model that enables analysis and design validation of an aircraft on-board electric taxiing system. A detailed model, which includes power electronics, electrical machine and mechanical drivetrain, is first developed and discussed. The model is then employed for simulating two characteristic taxiing mission profiles with a Boeing 737-400 as a selected benchmark aircraft. From the simulation findings, acceleration performance, power and energy load profiles, as well as the energy harvesting stages are studied. These outcomes allow to evaluate the appropriate energy storage technology to be selected, enabling complete emission free aircraft taxiing.
| Original language | English |
|---|---|
| Title of host publication | 2019 22nd International Conference on Electrical Machines and Systems, ICEMS 2019 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| ISBN (Electronic) | 9781728133980 |
| DOIs | |
| Publication status | Published - Aug 2019 |
| Event | 22nd International Conference on Electrical Machines and Systems, ICEMS 2019 - Harbin, China Duration: 11 Aug 2019 → 14 Aug 2019 |
Publication series
| Name | 2019 22nd International Conference on Electrical Machines and Systems, ICEMS 2019 |
|---|
Conference
| Conference | 22nd International Conference on Electrical Machines and Systems, ICEMS 2019 |
|---|---|
| Country/Territory | China |
| City | Harbin |
| Period | 11/08/19 → 14/08/19 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Free Keywords
- Electric taxiing
- double star PMSM
- modelling
ASJC Scopus subject areas
- Control and Optimization
- Energy Engineering and Power Technology
- Control and Systems Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering
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