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Robust Flutter Margin Analysis that Incorporates Flight DataAn approach for computing worst-case flutter margins has been formulated in a robust stability framework. Uncertainty operators are included with a linear model to describe modeling errors and flight variations. The structured singular value, mu, computes a stability margin that directly accounts for these uncertainties. This approach introduces a new method of computing flutter margins and an associated new parameter for describing these margins. The mu margins are robust margins that indicate worst-case stability estimates with respect to the defined uncertainty. Worst-case flutter margins are computed for the F/A-18 Systems Research Aircraft using uncertainty sets generated by flight data analysis. The robust margins demonstrate flight conditions for flutter may lie closer to the flight envelope than previously estimated by p-k analysis.
Document ID
19980041295
Acquisition Source
Armstrong Flight Research Center
Document Type
Technical Publication (TP)
Authors
Lind, Rick
(NASA Dryden Flight Research Center Edwards, CA United States)
Brenner, Martin J.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1998
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.60:206543
NASA/TP-1998-206543
H-2209
Report Number: NAS 1.60:206543
Report Number: NASA/TP-1998-206543
Report Number: H-2209
Funding Number(s)
PROJECT: RTOP 529-31-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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