Visual performance evaluation of helicopter pilots in vibrating cockpit

Aykut Tamer, Andrea Zanoni, Alessandro Cocco, Pierangelo Masarati

Research output: Chapter or section in a book/report/conference proceedingChapter in a published conference proceeding

1 Citation (SciVal)

Abstract

Rotorcraft are known to suffer from relatively high levels of vibration as compared to their fixed-wing counterpart, due to exposure to significant vibratory load levels. Pilots usually operate in a vibrating cockpit, and hence can suffer from degradation of their instrument reading performance. Therefore, the expected level of degradation in visual performance should be estimated when there is room for design changes. The present work demonstrates the evaluation of visual vibration degradation of helicopter pilots using a modular analysis environment. Core elements are an aeroelastic helicopter model, a seat-cushion model, a detailed human biodynamics multibody model, and a simplified model of ocular dynamics, which are assembled into an overall model. The contribution of each component is examined using a figure of merit that includes both eye and instrument panel vibration.

Original languageEnglish
Title of host publication15th International Conference on Multibody Systems, Nonlinear Dynamics, and Control
PublisherThe American Society of Mechanical Engineers(ASME)
ISBN (Electronic)9780791859261
DOIs
Publication statusPublished - 25 Nov 2019
EventASME 2019 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC-CIE 2019 - Anaheim, USA United States
Duration: 18 Aug 201921 Aug 2019

Publication series

NameProceedings of the ASME Design Engineering Technical Conference
Volume6

Conference

ConferenceASME 2019 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC-CIE 2019
Country/TerritoryUSA United States
CityAnaheim
Period18/08/1921/08/19

Bibliographical note

Funding Information:
The present work received partial support from Leonardo Helicopter Division. The authors particularly acknowledge LHD for providing part of the data used in the analysis.

Publisher Copyright:
Copyright © 2019 ASME.

ASJC Scopus subject areas

  • Mechanical Engineering
  • Computer Graphics and Computer-Aided Design
  • Computer Science Applications
  • Modelling and Simulation

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