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Support of Icing Flight Tests by Near Real-Time Data Analysis

Raab, Christian and Ohme, Per and Deiler, Christoph (2016) Support of Icing Flight Tests by Near Real-Time Data Analysis. Deutscher Luft- und Raumfahrtkongress 2016, 13. - 15. September 2016, Braunschweig.

Full text not available from this repository.

Abstract

Flight testing of aircraft with altered aerodynamic configuration is a safety-critical and time-consuming task. For the evaluation of the aircraft characteristics under SLD (supercooled large droplets) icing conditions, flight tests with artificial ice shapes were performed. These flight tests were supported by online algorithms for the estimation of aerodynamic parameters. Results were available in near real-time onboard the aircraft or already during the debriefing on ground. Pre-flight data from wind tunnel experiments could be confirmed already during the flight using these online analysis tools, thus the flight tests could be performed in shorter time and more safely. This paper will introduce the developed analysis tools and will present results from the flight test campaign.

Item URL in elib:https://elib.dlr.de/106152/
Document Type:Conference or Workshop Item (Speech)
Title:Support of Icing Flight Tests by Near Real-Time Data Analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Raab, Christianchristian.raab (at) dlr.deUNSPECIFIED
Ohme, PerPer.Ohme (at) dlr.deUNSPECIFIED
Deiler, Christophchristoph.deiler (at) dlr.deUNSPECIFIED
Date:13 September 2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Flight Test, Icing, Parameter Estimation, System Identification, Performance, Aerodynamic, Stability and Control
Event Title:Deutscher Luft- und Raumfahrtkongress 2016
Event Location:Braunschweig
Event Type:national Conference
Event Dates:13. - 15. September 2016
Organizer:DGLR
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 - Systems and Cabin
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By: Raab, Dipl.-Ing. Christian
Deposited On:22 Sep 2016 14:35
Last Modified:09 Mar 2017 15:29

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