Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-24453
Publication type: Article in scientific journal
Type of review: Peer review (publication)
Title: Atmospheric disturbance modelling for a piloted flight simulation study of airplane safety envelope over complex terrain
Authors: Liu, Xinying
Abà, Anna
Capone, Pierluigi
Manfriani, Leonardo
Fu, Yongling
et. al: No
DOI: 10.3390/aerospace9020103
10.21256/zhaw-24453
Published in: Aerospace
Volume(Issue): 9
Issue: 2
Page(s): 103
Issue Date: 2022
Publisher / Ed. Institution: MDPI
ISSN: 2226-4310
Language: English
Subjects: Flight safety; Large eddy simulation; Aviation meteorology; Real-time flight simulation; Mountainous terrain
Subject (DDC): 629: Aeronautical, automotive engineering
Abstract: A concept of a new energy management system synthesizing meteorological and orographic influences on airplane safety envelope was developed and implemented at the ZHAW Centre for Aviation. A corresponding flight simulation environment was built in a Research and Didactics Simulator (ReDSim) to test the first implementation of the cockpit display system. A series of pilot-in-the-loop flight simulations were carried out with a group of pilots. A general aviation airplane model Piper PA-28 was modified for the study. The environment model in the ReDSim was modified to include a new ad hoc subsystem simulating atmospheric disturbance. In order to generate highly resolved wind fields in the ReDsim, a well-established large-eddy simulation model, the Parallelized Large-Eddy Simulation (PALM) framework, was used in the concept study, focusing on a small mountainous region in Switzerland, not far from Samedan. For a more realistic representation of specific meteorological situations, PALM was driven with boundary conditions extracted from the COSMO-1 reanalysis of MeteoSwiss. The essential variables (wind components, temperature, and pressure) were extracted from the PALM output and fed into the subsystem after interpolation to obtain the values at any instant and any aircraft position. Within this subsystem, it is also possible to generate statistical atmospheric turbulence based on the widely used Dryden turbulence model. The paper compares two ways of generating atmospheric turbulence, by combining the numerical method with the statistical model and introduces the flight test procedure with an emphasis on turbulence realism; it then presents the experiment results including a statistical assessment achieved by collecting pilot feedback on turbulence characteristics and turbulence/task combination.
URI: https://digitalcollection.zhaw.ch/handle/11475/24453
Fulltext version: Published version
License (according to publishing contract): CC BY 4.0: Attribution 4.0 International
Departement: School of Engineering
Organisational Unit: Centre for Aviation (ZAV)
Published as part of the ZHAW project: Konzept und Machbarkeitstudie eines Leistungsreservenrechners für die allgemeine Luftfahrt
Appears in collections:Publikationen School of Engineering

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