Flutter suppression for the Active Flexible Wing - Control system design and experimental validation-Reference-Cited by-同舟云学术

Flutter suppression for the Active Flexible Wing - Control system design and experimental validation

Published:1992-04-16 Issue: Volume: Page:
ISSN:
Container-title:Dynamics Specialists Conference
language:
Short-container-title:

Author:

WASZAK M.¹,SRINATHKUMAR S.²

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. National Aeronautical Laboratory, Bangalore, India

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2097

Reference12 articles.

1. Adams,W.M., Christhilf,D.M.,Waszak,M.R.,Mukhopadhyay, V., and Srinathkurnar, S. "Design, Test, and Evaluationof Three Active Flutter Suppression Controllers," NASA TM4338,1992.

2. Buttrill,C.S.,Bacon,B.J. Heeg,J., Houck,J.A., andWood,D. "Simulation and Model Reduction for the AFW Program," AIAA Paper No. 92-2081. Presented at the Dynamic SpecialistsConference,Dallas, TX,April 16-17.1992.

3. Hot-bench simulation of the active flexible wing wind-tunnel model

4. The multiple-function multi-input/multi-output digital controller system for the AFW wind tunnel model

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