NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel DataA new method is presented for estimating frequency responses and their uncertainties from wind-tunnel data in real time. The method uses orthogonal phase-optimized multi- sine excitation inputs and a recursive Fourier transform with a least-squares estimator. The method was first demonstrated with an F-16 nonlinear flight simulation and results showed that accurate short period frequency responses were obtained within 10 seconds. The method was then applied to wind-tunnel data from a previous aeroelastic test of the Joined- Wing SensorCraft. Frequency responses describing bending strains from simultaneous control surface excitations were estimated in a time-efficient manner.
Document ID
20120014504
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Grauer, Jared A
(NASA Langley Research Center Hampton, VA, United States)
Heeg, Jennifer
(NASA Langley Research Center Hampton, VA, United States)
Morelli, Eugene A
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 26, 2013
Publication Date
August 13, 2012
Subject Category
Aircraft Stability And Control
Report/Patent Number
NF1676L-14035
Report Number: NF1676L-14035
Meeting Information
Meeting: 2012 AIAA Atmospheric Flight Mechanics Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 13, 2012
End Date: August 16, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.07.46.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available