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Impact of differential torsional rotor cant on the flight characteristics of a passenger-grade quadrotor

Atci, Kagan and Jusko, Tim and Strbac, Alexander and Güner, Feyyaz (2024) Impact of differential torsional rotor cant on the flight characteristics of a passenger-grade quadrotor. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-023-00705-7. ISSN 1869-5590.

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Official URL: https://link.springer.com/article/10.1007/s13272-023-00705-7

Abstract

At the Institute of Flight Systems at DLR, studies have been performed to understand the flight characteristics of novel eVTOL configurations. As part of these studies, previously conducted handling qualities assessments on a two-passenger quadrotor configuration had revealed major deficiencies about its yaw axis. Based on this result, the quadrotor model has been modified by differential torsional canting to improve its yaw characteristics. This paper analyzes the resulting impacts of such modification on the flight performance, dynamic stability and handling qualities. A piloted simulator test campaign was conducted to assess predicted and assigned handling qualities levels in compliance with the quantitative and qualitative performance standards of ADS-33E. The results show an improvement in midterm yaw response at the expense of increase in total required power. The pilot ratings and comments also confirm the improvement on the yaw response upon the flown MTEs.

Item URL in elib:https://elib.dlr.de/201757/
Document Type:Article
Title:Impact of differential torsional rotor cant on the flight characteristics of a passenger-grade quadrotor
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Atci, KaganUNSPECIFIEDhttps://orcid.org/0000-0002-4975-4458151091245
Jusko, TimUNSPECIFIEDhttps://orcid.org/0009-0004-7571-9906151091248
Strbac, AlexanderUNSPECIFIEDhttps://orcid.org/0000-0002-9660-5017151091249
Güner, FeyyazUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:4 January 2024
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1007/s13272-023-00705-7
Publisher:Springer
ISSN:1869-5590
Status:Published
Keywords:Urban air mobility, eVTOL, Multirotor, Quadrotor, Flight characteristics, handling qualities, rotor cant
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Rotorcraft and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Flight Systems
Deposited By: Atci, Kagan
Deposited On:19 Jan 2024 16:06
Last Modified:26 Jan 2024 09:36

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  • Impact of differential torsional rotor cant on the flight characteristics of a passenger-grade quadrotor. (deposited 19 Jan 2024 16:06) [Currently Displayed]

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