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Motion Cueing Optimisation Applied to Rotorcraft Flight Simulation

Jones, Michael (2017) Motion Cueing Optimisation Applied to Rotorcraft Flight Simulation. CEAS Aeronautical Journal, 8 (3), pp. 523-539. Springer. DOI: 10.1007/s13272-017-0256-1 ISSN 1869-5582

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Official URL: https://link.springer.com/article/10.1007/s13272-017-0256-1

Abstract

Achieving good motion cueing in rotorcraft flight simulation is a long-standing challenge in the simulation community. The current reliance upon subjective opinion leads to a wide range of motion configurations, which almost certainly do not offer the optimal level of vestibular cueing. Furthermore, without the understanding of the optimal motion settings, objective criteria are difficult to apply. This paper presents a new method designed to optimise and evaluate the response of any motion platform, based upon the input to the system and the given motion system constraints. The method is utilised to tune the motion platform of the air vehicle simulator. Results show promise for the use of the optimisation, as good fidelity is shown through pilot subjective comments and ratings.

Item URL in elib:https://elib.dlr.de/114471/
Document Type:Article
Title:Motion Cueing Optimisation Applied to Rotorcraft Flight Simulation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Jones, MichaelMichael.Jones (at) dlr.deUNSPECIFIED
Date:14 July 2017
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:8
DOI :10.1007/s13272-017-0256-1
Page Range:pp. 523-539
Publisher:Springer
ISSN:1869-5582
Status:Published
Keywords:Motion; Rotorcraft; Piloted Simulation; Optimisation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Smart Rotorcraft
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: Jones, Michael
Deposited On:10 Oct 2017 10:32
Last Modified:06 Sep 2019 15:24

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