Active control of flutter in compressible flow and its aeroelastic scaling

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 1, 2001, Pages 167-175

  Friedmann, P P ^a,b   Presente, E ^a,c  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b UNIVERSITY OF MICHIGAN   (United States)

^c Elbit Systems   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPRESSIBLE FLOW; CONSTRAINT THEORY; FEEDBACK CONTROL; KALMAN FILTERING; LINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS; STATE FEEDBACK;

AEROELASTIC SCALING; FLUTTER SUPPRESSIONS;

FLUTTER (AERODYNAMICS);

EID: 0034831746     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4698     Document Type: Article

References (37)

1. Noll, T. E., "Aeroservoelasticity," Flight-Vehicle Materials, Structures, and Dynamics - Assessment and Future Direction, edited by A. K. Noor and S. L. Venneri, Vol. 5, American Society of Mechanical Engineers, Fairfield, NJ, 1993, Chap. 3, pp. 179-212.
2. Livne, E., "Integrated Aeroservoelastic Optimization: Status and Direction," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 122-145.
3. Friedmann, P. P., "Renaissance of Aeroelasticity and Its Future," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 105-121.
4. Newsom, J. R., Pototzky, A. S., and Abel, I., "Design of a Flutter Suppression System for an Experimental Drone Aircraft," Journal of Aircraft, Vol. 22, No. 5, 1985, pp. 380-386.
5. Roger, K. L., Hodges, G. E., and Felt, L., "Active Flutter Suppression, A Flight Test Demonstration," Journal of Aircraft, Vol. 6, No. 12, 1975, pp. 551-556.
6. Edwards, J. W., "Unsteady Aerodynamic Modeling and Active Aeroelastic Control," Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA, Feb. 1977.
7. Roger, K. L., "Airplane Math Modeling Methods for Active Control Design," Structural Aspects of Active Controls, CP-228, AGARD, Aug. 1977, pp. 4-1-4-11.
8. Ehlers, S. M., and Weisshaar, T. A., "Static Aeroelastic Behavior of an Adaptive Laminated Piezoelectric Composite Wing," Proceedings of the 31st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA, Washington, DC, 1990, pp. 1611-1623.
9. Heeg, J., Scott, R. C., and McGowan, A.-M. R., "Aeroelastic Research Using Smart Structures Concepts," Aeroelasticity and Fluid Structure Interaction Problems, edited by P. P. Friedmann and J. C. I. Chang, AD-Vol. 44, American Society of Mechanical Engineers, Chicago, 1994, pp. 161-173.
10. Heeg, J., McGowan, A., Crawley, E., and Lin, C., "The Piezoelectric Aeroelastic Response Tailoring Investigation," International Forum on Aeroelasticity and Structural Dynamics 1995, Royal Aeronautical Society, Manchester, England, U.K., 1995, pp. 8.1-8.11.
11. Lazarus, K. B., Crawley, E. F., and Bohlmann, J. D., "Static Aeroelastic Control Using Strain Actuated Adaptive Structures," Journal of Intelligent Material Systems and Structures, Vol. 2, No. 3, 1991, pp. 386-410.
12. Lin, C. Y., "Towards Optimal Strain Actuated Aeroelastic Control," Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, Jan. 1996.
13. Lin, C. Y., Crawley, E. F., and Heeg, J., "Open- and Closed-Loop Results of a Strain-Actuated Active Aeroelastic Wing," Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 987-994.
14. Lazarus, K. B., Crawley, E. F., and Lin, C. Y., "Multivariable Active Lifting Surface Control Using Strain Actuation: Analytical and Experimental Results," Journal of Aircraft, Vol. 34, No. 3, 1997, pp. 313-321.
15. McGowan, A., Heeg, J., and Lake, R. C., "Results of Wind-Tunnel Testing from the Piezoelectric Aeroelastic Response Tailoring Investigation," Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, AIAA, Reston, VA, 1996, pp. 1722-1732.
16. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Addison-Wesley, Cambridge, MA, 1955.
17. Hunt, G. K., "Similarity Requirements for Aeroelastic Models of Helicopter Rotors," Aeronautical Research Council, CP 1245, Jan. 1973.
18. Regier, A. A., "The Use of Scaled Dynamic Models in Several Aerospace Vehicle Studies," Proceedings of ASME Colloquium on the Use of Models and Scaling in Simulation of Shock and Vibration, American Society of Mechanical Engineers, New York, 1963, pp. 34-50.
19. Baker, W. E., Westine, P. S., and Dodge, F. T., Similarity Methods in Engineering Dynamics: Theory and Practice of Scale Modeling, rev. ed., Elsevier, New York, 1991.
20. Theodorsen, T., "General Theory of Aerodynamic Instability and the Mechanism of Flutter," NACA TR 496, 1935.
21. Albano, E., and Rodden, W. P., "Doublet-Lattice Method for Calculating Lift Distribution on Oscillating Surfaces in Subsonic Flows," AIAA Journal, Vol. 7, No. 2, 1969, pp. 279-282.
22. Mukhopadhyay, V., "Flutter Suppression Control Law Design and Testing for the Active Flexible Wing," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 45-51.
23. Kwakernaak, H., and Sivan, R., Linear Optimal Control Systems, Wiley, New York, 1972.
24. Dowell, E. H., A Modern Course in Aeroelasticity, 3rd ed., Kluwer Academic, Norwell, MA, 1995, Chap. 12.
25. Potter, J. E., "Matrix Quadratic Solutions," SIAM Journals on Applied Mathematics, Vol. 14, No. 3, 1966, pp. 496-501.
26. Bryson, A. E., Jr., and Ho, Y. C., Applied Optimal Control, Hemisphere, Washington, DC, 1975.
27. Roy, I. D., and Eversman, W., "Adaptive Flutter Suppression of an Unswept Wing," Journal of Aircraft, Vol. 33, No. 4, 1996, pp. 775-783.
28. Friedmann, P. P., Guillot, D., and Presente, E. H., "Adaptive Control of Aeroelastic Instabilities in Transonic Flow and Its Scaling," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1190-1199.
29. Eversman, W., and Roy, I. D., "Active Flutter Suppression Using Multi-Input/Multi-Output Adaptive Least Mean Square Control," Journal of Aircraft, Vol. 34, No. 2, 1997, pp. 244-250.
30. Kuethe, A. M., and Chow, C., Foundations of Aerodynamics, 4th ed. Wiley, New York, 1986.
31. Lazarus, K. B., "Multivariable High-Authority Control of Plate-Like Active Lifting Surfaces," Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, June 1992.
32. Shames, I. H., and Dym, C. L., Energy and Finite Element Methods in Structural Mechanics, Taylor and Francis, Washington, DC, 1985.
33. Presente, E., "Innovative Scaling Laws for Aeroelastic and Aeroservoelastic Problems in Compressible Flow," Ph.D. Dissertation, Mechanical and Aerospace Engineering Dept., Univ. of California, Los Angeles, 1999.
34. Theodorsen, T., and Garrick, I. E., "Nonstationary Flow About a Wing-Aileron-Tab Combination Including Aerodynamic Balance," NACA TR 736, May, 1942,
35. Raymer, D. P., Aircraft Design: A Conceptual Approach, 2nd ed., AIAA Education Series, AIAA, Washington, DC, 1992.
36. Nicolai, L. M., Fundamentals of Aircraft Design, METS, Inc., San Jose, CA, 1984.
37. Reich, G. W., van Schoor, M. C., Lin, C. Y., and Crawley, E. F., "An Active Aeroelastic Wing Model for Vibration and Flutter Suppression," Proceedings of the 36th AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA, Washington, DC, 1995, pp. 314-324.