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Aerodynamic model identification of Frauke UAV

Lombaerts, Thomas (2012) Aerodynamic model identification of Frauke UAV. AIAA 2012 Atmospheric Flight Mechanics Conference and Exhibit, 13-16 Aug 2012, Minneapolis, Minnesota, USA.

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Official URL: http://pdf.aiaa.org/getfile.cfm?urlX=6%3A7I%276D%26X%5BRO%23R%20%23JP4S%5EQ%3AG%224%2AX%24%5F0%20%20%0A&urla=%26%2A%22%5C%21%23%20NF%0A&urlb=%21%2A%20%20%20%0A&urlc=%21%2A%20%20%20%0A&urld=%28%2A%22P%25%21PJGT18%20%0A&urle=%28%2A%22H%23%22%40NBUQ%3C%20%0A


This paper describes the methods and results of an identification campaign, which has been set up for the mini UAV Frauke. The estimated parameter values will be used to elaborate an accurate non-linear simulation model of the UAV, which will subsequently be used to develop model based non-linear control techniques for the vehicle. The identification procedure has been performed with the so-called two step method. First, the aircraft states are estimated based upon the aircraft kinematics, after which the aerodynamic model parameters are identified. It has been found that, due to the dynamic behaviour of the UAV, a more extended aerodynamic model including nonlinear terms is needed. Residual analysis confirms the accuracy of the obtained results.

Item URL in elib:https://elib.dlr.de/77277/
Document Type:Conference or Workshop Item (Paper)
Title:Aerodynamic model identification of Frauke UAV
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Lombaerts, Thomasthomas.lombaerts (at) dlr.deUNSPECIFIED
Date:13 August 2012
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:aircraft model identification, UAV, two step method, aircraft state estimation, flight path reconstruction, nonlinear aerodynamic model, model structure selection, parameter estimation, parameter identification, residual analysis
Event Title:AIAA 2012 Atmospheric Flight Mechanics Conference and Exhibit
Event Location:Minneapolis, Minnesota, USA
Event Type:international Conference
Event Dates:13-16 Aug 2012
Organizer:American Institute of Aeronautics and Astronautics AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Lombaerts, Dr Thomas
Deposited On:17 Sep 2012 13:43
Last Modified:03 Dec 2012 09:40

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