Flutter suppression using micro-trailing edge effectors

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 7, Issue , 2003, Pages 4915-4924

  Bieniawski, Stefan ^a   Kroo, Ilan M ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; ASPECT RATIO; CONTROL EQUIPMENT; MATHEMATICAL MODELS; WINGS;

CLOSED LOOP TESTING; FLUTTER SUPPRESSION; MICROTRAILING EDGE EFFECTORS; REINFORCEMENT LEARNING POLICY SEARCH TECHNIQUES;

FLUTTER (AERODYNAMICS);

EID: 0042978664     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1941     Document Type: Conference Paper

References (19)

1. Nae, C., "Synthetic Jet Influence on NACA 0012 Airfoil at High Angles of Attack," AIAA Paper 98-4523.
2. Seifert, A., Darabi, A., Wygnanski, I., "Delay of Airfoil Stall by Periodic Excitation," Journal of Aircraft, Vol. 32, No. 4, July-August 1996.
3. Kroo, I., Eaton, J., Prinz, F., "UAV Aeroelastic Control Using Redundant Microflaps," Air Force Office of Scientific Research Program Review for Year I, 1999.
4. Solovitz, S., Eaton, J.K., "Aeroelastic Control Using Redundant Microactuators," 3rd ASME/JSME Joint Fluids Engineering Conference, July 18-23, 1999, San Francisco, CA.
5. Kroo, I., Bieniawski, S., "UAV Aeroelastic Control Using Redundant Micro-Actuators," Air Force Office of Scientific Research Program in Turbulence and Rotating Flows 2001 Contractor's Meeting, August 13-14, 2001, Seattle, WA.
6. Liebeck, R. H., "Design of Subsonic Airfoils for High Lift," Journal of Aircraft, Vol. 15, No. 9, Sept., 1978.
7. Jeffrey, D., Zhang, X., and Hurst, D.W., "Aerodynamics of Gurney Flaps on a Single-Element High-Lift Wing," Journal of Aircraft, Vol. 37, No. 2, 2000, pp. 295-301.
8. Storms, B. L. and Jang, C. S., "Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators," Journal of Aircraft, Vol. 31, No. 3, June 1994.
9. Jang, C.S., Ross, J. C., and Cummings, R. M., "Computational Evaluation of an Airfoil with a Gurney Flap", AIAA Paper 92-2708, June 1992.
10. Kroo, I. "Aerodynamic Concepts for Future Aircraft," 30th AIAA Fluid Dynamics Conference (AIAA 99-3524), Norfolk, Va, June-July 1999.
11. Lee, H., Kroo, I., Bieniawski, S., "Flutter Suppression for High Aspect Ratio Flexible Wings Using Microflaps," AIAA 2002-1717, April 2002.
12. Jensen, D. W., Crawley, E.F., Dugundji, J., "Vibration of Cantilevered Graphite/Epoxy Plates with Bending-Torsion Coupling," Journal of Reinforced Plastics and Composites, Vol. 1, July 1982, pp. 254-269.
13. Hollowell, S.J., and Dugundji, J., "Aeroelastic Flutter and Divergence of Stiffness Coupled, Graphite Epoxy Cantilevered Plates," Journal of Aircraft, Vol. 21, Jan 1984, pp 69-76.
14. Landsberger, B., and Dugundji, J., "Experimental Aeroelastic Behavior of Unswept and Forward Swept Graphite/Epoxy Wings," Journal of Aircraft, Vol. 22, Aug 1985, pp 679-686.
15. Theodorsen, T., "General Theory of Aerodynamic Instability and the Mechanism of Flutter," NACA TR 496, 1935.
16. Bryson, A. Control of Spacecraft and Aircraft, Princeton University Press, Princeton, New Jersey, 1994.
17. Richard Sutton and Andrew Barto, Reinforcement Learning: An introduction. MIT Press, 1998
18. Ng, Andrew Y., and Jordon, Michael, "PEGASUS: A policy search method for large MDPs and POMDPs." In Uncertainty in Artificial Intelligence, Proceedings of the Sixteenth Conference, 2000.
19. Schneider, J.G., and Bagnell, J.A., "Autonomous Helicopter Control Using Reinforcement Learning Policy Search Methods," Proceedings of the International Conference on Robotics and Automation, May 2001.