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Process, methods and tools for flexible aircraft flight dynamics model integration

Kier, Thiemo und Looye, Gertjan und Scharpenberg, Moriz und Reijerkerk, Marianne (2007) Process, methods and tools for flexible aircraft flight dynamics model integration. International Forum on Aeroelasticity and Structural Dynamics, Stockholm (Schweden).

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Kurzfassung

Multi-disciplinary flight dynamics models for rigid and flexible aircraft are used in various areas and stages of the aircraft design process, like for example flight loads analysis and flight control law design. These models must be sufficiently accurate, but also allow for thousands of simulations in a reasonable amount of time (i.e. ’loop-capable’). Depending on the application, flight dynamics models need to be available in various forms, like ODEs for nonlinear simulation, linear state space models for control analysis, etc. A major challenge in development of multi-disciplinary flight dynamics models is the handling and integration of data from various sources, removing overlaps, and filling in gaps in case specific data is missing. During the last decade, the DLR Institute of Robotics and Mechatronics has developed methods and tools for these tasks, as well as for model implementation in various forms suitable for aircraft design analysis. Recently, these aspects have been integrated in a standardized efficient model integration process, called DAMIP (DLR Aircraft Model Integration Process). DAMIP uses the data structure of VarLoads, which is developed in cooperation with Airbus, and is backed by appropriate methods and tools. In this paper an overview of DAMIP will be given, as well as some recent application examples.

Dokumentart:Konferenzbeitrag (Vortrag, Paper)
Titel:Process, methods and tools for flexible aircraft flight dynamics model integration
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID
Kier, ThiemoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Looye, GertjanNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Scharpenberg, MorizNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Reijerkerk, MarianneNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2007
Referierte Publikation:Ja
In Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Multi-disciplinary Modelling, Simulation, Loads Analysis, Flight Control Law Design, Aeroelasticity
Veranstaltungstitel:International Forum on Aeroelasticity and Structural Dynamics
Veranstaltungsort:Stockholm (Schweden)
Veranstaltungsart:internationale Konferenz
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Starrflügler (alt)
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Starrflüglerforschung
DLR - Teilgebiet (Projekt, Vorhaben):L - Systeme & Kabine (alt)
Standort: Oberpfaffenhofen
Institute & Einrichtungen:Institut für Robotik und Mechatronik (bis 2012) > Systemdynamik und Regelungstechnik (war Entwurfsorientierte Regelungstechnik)
Hinterlegt von: Klauer, Monika
Hinterlegt am:20 Okt 2008
Letzte Änderung:12 Dez 2013 20:33

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