Conference Paper/Proceeding/Abstract 527 views
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation
AIAA SCITECH 2023 Forum
Swansea University Author:
Ye Yuan
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DOI (Published version): 10.2514/6.2023-2206
Abstract
The manoeuvrability of the Urban Air Mobility (UAM) determines its handling qualities and safety. However, this novel rotor-powered vehicle configuration has unique characteristics, including the complicated aerodynamic interference of the multi-rotor systems, the transition mode that may alter the...
Published in: | AIAA SCITECH 2023 Forum |
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Published: |
Reston, Virginia
American Institute of Aeronautics and Astronautics
2023
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Online Access: |
http://dx.doi.org/10.2514/6.2023-2206 |
URI: | https://cronfa.swan.ac.uk/Record/cronfa63019 |
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v2 63019 2023-03-24 Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation cdadbd9e334ad914d7968a538d9522a4 0000-0002-7568-0130 Ye Yuan Ye Yuan true false 2023-03-24 GENG The manoeuvrability of the Urban Air Mobility (UAM) determines its handling qualities and safety. However, this novel rotor-powered vehicle configuration has unique characteristics, including the complicated aerodynamic interference of the multi-rotor systems, the transition mode that may alter the rotor wake significantly, and the multiple redundant controllers. These features make it harder to quantify its manoeuvrability. Therefore, a series of novel modelling and assessment methods are developed in this article to assess the manoeuvrability of UAM vehicles. First, the universal UAM flight simulation modelling method is delivered based on the multi-agent simulation engine, providing accurate flight dynamics estimates for different UAM configurations. Then, the Two Timescale Integration method is incorporated into the inverse simulation, enabling this method to tackle the non-minimum phase characteristics widely in the UAM system. Lastly, the deceleration,pop-down, normal landing, and emergency landing manoeuvres are mathematically defined, aiming at testing the manoeuvrability of the exampled UAM vehicles. The results indicated that the handling qualities during various manoeuvres are different, and the analysis also provides some suggestions on the UAM safety improvement. Meanwhile, the results demonstrated that the improved inverse simulation method could deal with the non-minimum phase features, allowing this method to analyse the UAM manoeuvrability across the flight envelope. Conference Paper/Proceeding/Abstract AIAA SCITECH 2023 Forum American Institute of Aeronautics and Astronautics Reston, Virginia Urban Air Mobility, Flight Dynamics, Tiltrotor Aircraft, Handling Qualities, Rotor Systems, Aerodynamic Characteristics, Emergency Landing, Flight Simulation, Flight Envelope, Aircraft Configurations 23 1 2023 2023-01-23 10.2514/6.2023-2206 http://dx.doi.org/10.2514/6.2023-2206 COLLEGE NANME General Engineering COLLEGE CODE GENG Swansea University Not Required 2023-04-26T10:33:22.1081116 2023-03-24T15:17:09.2148755 Faculty of Science and Engineering School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering Ye Yuan 0000-0002-7568-0130 1 Douglas Thomson 2 David Anderson 3 |
title |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation |
spellingShingle |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation Ye Yuan |
title_short |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation |
title_full |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation |
title_fullStr |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation |
title_full_unstemmed |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation |
title_sort |
Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation |
author_id_str_mv |
cdadbd9e334ad914d7968a538d9522a4 |
author_id_fullname_str_mv |
cdadbd9e334ad914d7968a538d9522a4_***_Ye Yuan |
author |
Ye Yuan |
author2 |
Ye Yuan Douglas Thomson David Anderson |
format |
Conference Paper/Proceeding/Abstract |
container_title |
AIAA SCITECH 2023 Forum |
publishDate |
2023 |
institution |
Swansea University |
doi_str_mv |
10.2514/6.2023-2206 |
publisher |
American Institute of Aeronautics and Astronautics |
college_str |
Faculty of Science and Engineering |
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|
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facultyofscienceandengineering |
hierarchy_top_title |
Faculty of Science and Engineering |
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facultyofscienceandengineering |
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Faculty of Science and Engineering |
department_str |
School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Aerospace, Civil, Electrical, General and Mechanical Engineering - Aerospace Engineering |
url |
http://dx.doi.org/10.2514/6.2023-2206 |
document_store_str |
0 |
active_str |
0 |
description |
The manoeuvrability of the Urban Air Mobility (UAM) determines its handling qualities and safety. However, this novel rotor-powered vehicle configuration has unique characteristics, including the complicated aerodynamic interference of the multi-rotor systems, the transition mode that may alter the rotor wake significantly, and the multiple redundant controllers. These features make it harder to quantify its manoeuvrability. Therefore, a series of novel modelling and assessment methods are developed in this article to assess the manoeuvrability of UAM vehicles. First, the universal UAM flight simulation modelling method is delivered based on the multi-agent simulation engine, providing accurate flight dynamics estimates for different UAM configurations. Then, the Two Timescale Integration method is incorporated into the inverse simulation, enabling this method to tackle the non-minimum phase characteristics widely in the UAM system. Lastly, the deceleration,pop-down, normal landing, and emergency landing manoeuvres are mathematically defined, aiming at testing the manoeuvrability of the exampled UAM vehicles. The results indicated that the handling qualities during various manoeuvres are different, and the analysis also provides some suggestions on the UAM safety improvement. Meanwhile, the results demonstrated that the improved inverse simulation method could deal with the non-minimum phase features, allowing this method to analyse the UAM manoeuvrability across the flight envelope. |
published_date |
2023-01-23T10:33:21Z |
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1764230798910685184 |
score |
11.021648 |