Control Synthesis with Load Minimization for the F/A-18 Active Aeroelastic
Wing (AAW)
- Collaborators
- Marty Brenner, NASA Dryden Flight Research Center
- Publications
-
R. Lind, D. Voracek, R. Truax, T. Doyle, S. Potter, and M. Brenner, ``A Flight Test to Demonstrate Flutter and Evaluate
the Flutterometer,'' The Aeronautical Journal, in review.
-
R. Lind,
``Flight Testing with the
Flutterometer,''
Journal of Aircraft, accepted for publication.
-
R. Lind,
``Flight Test Evaluation of
Flutter Prediction Methods'' ,
Journal of Aircraft, accepted for publication.
-
R. Lind and M. Brenner,
``Flutterometer : An On-Line Tool
to
Predict Robust Flutter Margins,''
Journal of Aircraft, Vol. 37, No. 6, November-December 2000,
pp. 1105-1112.
-
J.P. Mortagua and R. Lind, ``Accurate Flutterometer Predictions
using Volterra Modeling with Modal Parameter Estimation,''
submitted to AIAA Structures, Structural Dynamics, and
Materials Conference, to appear April 2003.
-
R. Lind, ``Flight Testing with the Flutterometer,'' International
Forum on Aeroelasticity and Structural Dynamics, Madrid, Spain, June 2001, Vol. 3, pp. 237-248.
-
R. Lind, ``Flight Testing with the Flutterometer,'' AIAA
Structures, Structural Dynamics, and Materials Conference,
Seattle WA, AIAA-01-1654, April 2001.