Advances in aircraft system identification at NASA Langley Research Center are discussed. The relevant time period includes the years since the last summary paper of this kind, which was published in the Journal of Aircraft in 2005. Research advances were achieved in flight test experiment design, frequency-domain modeling, real-time autonomous global modeling, rapid simulation development and updating, dynamic modeling in turbulence, flight data corrections, model uncertainty characterization, and aeroelastic modeling using distributed sensing. Possible future developments in the field are identified.
Advances in Aircraft System Identification at NASA Langley Research Center
Journal of Aircraft ; 60 , 5
2023-04-16
Miscellaneous
No indication
English
Flight test experiment design , Aircraft Design, Testing and Performance , Dynamic modeling in turbulence , Frequency-domain modeling , NASA Langley , Aircraft system identification , Model uncertainty characterization , Aeroelastic modeling , Global modeling , Real-time computing , Flight testing , Simulation updating
NTRS | 2008
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