Free flight wind tunnel tests for parameter identification

Nowack, Jan; Alles, Wolfgang

doi:910005761

Free flight wind tunnel tests for parameter identification

Nowack, Jan (Author) ; Alles, Wolfgang (Author)

2009

Konferenz/Event:VSDIA 2008 : 11th MINI Conference on Vehicle System Dynamics, Identification and Anomalies ; Budapest, Hungary 10-12 November, 2008

ImpressumAachen : Publikationsserver der RWTH Aachen University

Online
URN: urn:nbn:de:hbz:82-opus-27254
URL: https://publications.rwth-aachen.de/record/98532/files/2725.pdf

Einrichtungen

Lehrstuhl für Flugdynamik und Institut für Luft- und Raumfahrt (415410)

Inhaltliche Beschreibung (Schlagwörter)
Identifikation (Genormte SW) ; Simulation (Genormte SW) ; MATLAB (Genormte SW) ; SIMULINK (Genormte SW) ; Windkanal (Genormte SW) ; Ingenieurwissenschaften (frei) ; Identifizierung (frei) ; nichtlineare dynamische Inversion (frei) ; dSPACE (frei) ; identification (frei) ; simulation (frei) ; nonlinear dynamic inversion (frei) ; Pseudo Control Hedging (frei) ; wind tunnel (frei)

Thematische Einordnung (Klassifikation)
DDC: 620

Kurzfassung
The Chair of Flight Dynamics at the RWTH Aachen University is conducting research on a method for identification of flight mechanical characteristics on free flying models in a wind tunnel. The main goal is to create a eproducible free flight environment for cost effective identification of important values even in an early design stage. The method will combine the advantages of free flight with wind tunnel techniques as it takes the free flight into a reproducible environment under laboratory conditions. The paper gives an overview of the project and provides insight into the work done so far.

Fulltext:
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