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Conference Paper/Proceeding/Abstract 1004 views

Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation

Ye Yuan, Douglas Thomson, David Anderson

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...

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Published in: AIAA SCITECH 2023 Forum
Published: Reston, Virginia American Institute of Aeronautics and Astronautics 2023
Online Access: http://dx.doi.org/10.2514/6.2023-2206
URI: https://cronfa.swan.ac.uk/Record/cronfa63019
first_indexed 2023-03-24T15:21:19Z
last_indexed 2024-11-15T18:00:45Z
id cronfa63019
recordtype SURis
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spelling 2023-04-26T10:33:22.1081116 v2 63019 2023-03-24 Manoeuverability Assessment for Urban Air Mobility Using the Improved Inverse Simulation cdadbd9e334ad914d7968a538d9522a4 Ye Yuan Ye Yuan true false 2023-03-24 ACEM 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 Aerospace, Civil, Electrical, and Mechanical Engineering COLLEGE CODE ACEM 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 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
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title 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 2023-01-23T11:12:41Z
_version_ 1850847749111545856
score 11.08895

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