Kuchar, Richard (2017) Open Innovation/Sagitta – Implementation and Validation of a Real-Time Flight Dynamics model for Simulation, Integration Testing and Pilot Training. In: Workshop der ASIM/GI Fachgruppen STS und GMMS, AR 53, Seiten 61-68. ARGESIM Verlag Wien. ASIM/GI Workshop, 2017-03-09 - 2017-03-10, Ulm, Deutschland. ISBN 978-3-901608-50-6.
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Kurzfassung
The OpenInnovation/Sagitta project has its focus on the contribution of innovative technologies for the application within the UAV sector. Therein a number of research facilities and academic institutions – under the lead management of Airbus Defence and Space – are working together in order to resolve relevant questions: The Technical University of Munich (TUM), the University of the Armed Forces Munich (UniBW), the Technische Hochschule Ingolstadt (THI) and the TU Chemnitz (TUC), as well as the German Aerospace Center (DLR, being involved with a total of three institutes). Within project scope, a scaled demonstrator UAV aircraft has been designed for in-flight verification capabilities of the derived scientific project results. Aside the overall integration tasks in advance of its maiden flight, the aircraft is currently undergoing intensive simulation and integration testing activities on various levels. Within this paper, an overview of the general setup for these activities is given - specifically focusing on the required flight dynamics model (FDM) which depict the actual physical properties of the aircraft. Furthermore the respective implementation challenges due to project requirements are discussed in detail. Finally the performed validation tasks are described - as required to achieve clearance of the FDM for formal testing.
elib-URL des Eintrags: | https://elib.dlr.de/118439/ | ||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||
Titel: | Open Innovation/Sagitta – Implementation and Validation of a Real-Time Flight Dynamics model for Simulation, Integration Testing and Pilot Training | ||||||||
Autoren: |
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Datum: | 9 März 2017 | ||||||||
Erschienen in: | Workshop der ASIM/GI Fachgruppen STS und GMMS | ||||||||
Referierte Publikation: | Nein | ||||||||
Open Access: | Nein | ||||||||
Gold Open Access: | Nein | ||||||||
In SCOPUS: | Nein | ||||||||
In ISI Web of Science: | Nein | ||||||||
Band: | AR 53 | ||||||||
Seitenbereich: | Seiten 61-68 | ||||||||
Herausgeber: |
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Verlag: | ARGESIM Verlag Wien | ||||||||
Name der Reihe: | ARGESIM Report | ||||||||
ISBN: | 978-3-901608-50-6 | ||||||||
Status: | veröffentlicht | ||||||||
Stichwörter: | Simulation and Integration Testing, Sagitta UAV, Hardware-in-the-Loop, Flightdynamics Model | ||||||||
Veranstaltungstitel: | ASIM/GI Workshop | ||||||||
Veranstaltungsort: | Ulm, Deutschland | ||||||||
Veranstaltungsart: | Workshop | ||||||||
Veranstaltungsbeginn: | 9 März 2017 | ||||||||
Veranstaltungsende: | 10 März 2017 | ||||||||
Veranstalter : | ASIM/GI Fachgruppen STS, GMMS und Hochschule Ulm | ||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||
HGF - Programm: | Luftfahrt | ||||||||
HGF - Programmthema: | Flugzeuge | ||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Militärische Technologien (alt) | ||||||||
Standort: | Oberpfaffenhofen | ||||||||
Institute & Einrichtungen: | Institut für Systemdynamik und Regelungstechnik > Flugzeug-Systemdynamik | ||||||||
Hinterlegt von: | Kuchar, Richard | ||||||||
Hinterlegt am: | 23 Jan 2018 16:56 | ||||||||
Letzte Änderung: | 24 Apr 2024 20:22 |
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