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Time Domain Output Error System Identification of Iced Aircraft Aerodynamics

Deiler, Christoph (2015) Time Domain Output Error System Identification of Iced Aircraft Aerodynamics. Deutscher Luft- und Raumfahrtkongress 2015, 22.-24. Sep. 2015, Rostock.

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Abstract

A delta-model approach to characterize changed aircraft dynamics due to icing is analytically derived and its parameters are estimated. The model extension is formulated as a separate module in the aircraft flight mechanics simulation and can be used in existing simulation models. The application of the output error method in time domain allows to satisfactorily match model outputs and measurements as well as calculated aerodynamic derivatives. Using available flight data of a light business jet with different ice accumulation cases provided by EMBRAER, model parameters of the delta-model are determined and interpreted pertaining to the aerodynamic degradation caused by icing. The results show good promise, that the combination of modeling approach and estimation technique could be applicable to extend existing simulator models providing a basis for pilot training under icing conditions.

Item URL in elib:https://elib.dlr.de/98485/
Document Type:Conference or Workshop Item (Speech)
Title:Time Domain Output Error System Identification of Iced Aircraft Aerodynamics
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Deiler, ChristophFT-FDSUNSPECIFIED
Date:September 2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:System identification, parameter estimation, aircraft icing, performance degradation,
Event Title:Deutscher Luft- und Raumfahrtkongress 2015
Event Location:Rostock
Event Type:international Conference
Event Dates:22.-24. Sep. 2015
Organizer:Deutsche Gesellschaft für Luft- und Raumfahrt
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By: Deiler, Christoph
Deposited On:06 Oct 2015 14:36
Last Modified:06 Oct 2015 14:36

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  • Time Domain Output Error System Identification of Iced Aircraft Aerodynamics. (deposited 06 Oct 2015 14:36) [Currently Displayed]

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