Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel Data
Author(s) -
Jared A. Grauer,
Jennifer Heeg,
Eugene A. Morelli
Publication year - 2012
Publication title -
aiaa atmospheric flight mechanics conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2012-4641
Subject(s) - aeroelasticity , wind tunnel , wing , computer science , fixed wing , frequency response , aerodynamics , structural engineering , acoustics , engineering , aerospace engineering , physics , electrical engineering
A new method is presented for estimating frequency responses and their uncertainties from wind-tunnel data in real time. The method uses orthogonal phase-optimized multisine excitation inputs and a recursive Fourier transform with a least-squares estimator. The method was rst demonstrated with an F-16 nonlinear ight simulation and results showed that accurate frequency responses of the short period mode 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-ecient manner.
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