Nonlinear adaptive control of an aeroelastic two-dimensional lifting surface

Journal of Guidance, Control, and Dynamics

Volumn 29, Issue 2, 2006, Pages 382-390

  Behal, A ^a,b,c   Marzocca, P ^a,b,c   Rao, V M ^a   Gnann, A ^a,c  

^a CLARKSON UNIVERSITY   (United States)

^b Department of Electrical and Computer Engineering ^*

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CONTROL SYSTEM ANALYSIS; FEEDBACK CONTROL; FLUTTER (AERODYNAMICS); INCOMPRESSIBLE FLOW; OSCILLATIONS; PHASE INTERFACES;

AEROELASTIC TWO-DIMENSIONAL LIFTING SURFACE; INCOMPRESSIBLE FLOWFIELD; NONLINEAR ADAPTIVE CONTROL; ZERO DYNAMICS;

NONLINEAR CONTROL SYSTEMS;

EID: 33645575966     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.14011     Document Type: Article

References (38)

1. Dowell, E. H., A Modern Course in Aeroelasticity, Sijthoff and Noordhoff, 1978.
2. Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Lifting Surfaces to Gust and Arbitrary Explosive Loading Signature," International Journal of Impact Engineering, Vol. 25, No. 1, 2001, pp. 41-65.
3. Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelasticity of Two-Dimensional Lifting Surfaces via Indicial Function Approach," Aeronautical Journal, Vol. 106, No. 1056, 2002, pp. 147-153.
4. Marzocca, P., Librescu, L., and Silva, W. A., "Nonlinear Open-/Closed-Loop Aeroelastic Analysis of Airfoils via Volterra Series," AIAA Journal, Vol. 42, No. 4, 2004, pp. 673-686.
5. Vipperman, J. S., Clark, R. L., Conner, M. D., and Dowell, E. H., "Investigation of the Experimental Active Control of a Typical Section Airfoil Using a Trailing-Edge Flap," Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 224-229.
6. Lazaraus, K., Crawley, E., and Lin, C., "Fundamental Mechanisms of Aeroelastic Control with Control Surface and Strain Actuation," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 1, 1995, pp. 10-17.
7. Mukhopadhyay, V. (ed.), "Benchmark Active Control Technology," Pt. 1, Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 913-960.
8. Mukhopadhyay, V. (ed.), "Benchmark Active Control Technology," Pt. 2, Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1093-1139.
9. Mukhopadhyay, V. (ed.), "Benchmark Active Control Technology," Pt. 3, Journal of Guidance, Control, and Dynamics, Vol. 24, No. 1, 2001, pp. 146-192.
10. Mukhopadhyay, V., "Historical Perspective on Analysis and Control of Aeroelastic Responses," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 5, 2003, pp. 673-684.
11. Yuan, Y., Yu, P., Librescu, L., and Marzocca, P., "Aeroelasticity of Time-Delayed Feedback Control of Two-Dimensional Supersonic Lifting Surfaces," Journal of Guidance, Control, and Dynamics, Vol. 27, No, 5, 2004, pp. 795-803.
12. Dowell, E. H., Edwards, J., and Strganac, T., "Nonlinear Aeroelasticity," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 857-874.
13. Jones, D. J., and Lee, B. H. K., "Time Marching Numerical Solution of the Dynamic Response of Nonlinear Systems," National Aeronautical Establishment, Aeronautical Note-25, National Research Council, Ottawa, 1985.
14. Friedmann, P., Guillot, D., and Presente, E., "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.
15. Lind, R., and Brenner, M., Robust Aeroservoelastic Stability Analysis, Springer-Verlag, London, 1999.
16. Barker, J. M., and Balas, G. J., "Comparing Linear Parameter-Varying Gain-Scheduled Control Techniques for Active Flutter Suppression," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 948-955.
17. Scott, R. C., and Pado, L. E., "Active Control of Wind-Tunnel Model Aeroelastic Response Using Neural Networks," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1100-1108.
18. Guillot, D. M., and Friedmann, P. P., "Fundamental Aeroservoelastic Study Combining Unsteady Computational Fluid Mechanics with Adaptive Control," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1117-1126.
19. Ko, J., Kurdila, A. J., and Strganac, T. W., "Nonlinear Control of a Prototypical Wing Section with Torsional Nonlinearity," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 6, 1997, pp. 1181-1189.
20. Ko, J., and Strganac, T. W., "Stability and Control of a Structurally Non-linear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 5, 1998, pp. 718-725.
21. Ko, J., Strganac, T. W., and Kurdila, A. J., "Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity," Nonlinear Dynamics, Vol. 18, No. 3, 1999, pp. 289-301.
22. Zeng, Y., and Singh, S. N., "Output Feedback Variable Structure Adaptive Control of an Aeroelastic Systems," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 830-837.
23. Singh, S. N., and Wang, L., "Output Feedback Form and Adaptive Stabilization of a Nonlinear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4, 2002, pp. 725-732.
24. Xing, W., and Singh, S. N., "Adaptive Output Feedback Control of a Nonlinear Aeroelastic Structure," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1109-1116.
25. Zhang, R., and Singh, S. N., "Adaptive Output Feedback Control of an Aeroelastic System with Unstructured Uncertainties," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 3, 2001, pp. 502-509.
26. Scanlan, R. H., and Rosenbaum, R., Introduction to the Study of Aircraft Vibration and Flutter, Macmillan, New York, 1951.
27. Edwards, J. W., "Unsteady Aerodynamic Modeling and Active Aeroelastic Control," Guidance and Control Lab., Dept, of Aeronautics and Astronautics, SUDARR 504, Stanford Univ., Stanford, CA, Feb. 1977;
28. also NASA CR-148019, 1977.
29. Block, J. J., and Strganac, T. W., "Applied Active Control for a Non-linear Aeroelastic Structure," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 838-845.
30. Fung, Y. C., An Introduction to the Theory of Aeroelasticity, Dover, New York, 1955.
31. Leishman, J. G., "Unsteady Lift of an Airfoil with a Trailing-Edge Flap Based on Indicial Concepts," Journal of Aircraft, Vol. 31, No. 2, 1994, pp. 288-297.
32. Leishman, J. G., "Validation of Approximate Indicial Aerodynamic Functions for Two-Dimensional Subsonic Flow," Journal of Aircraft, Vol. 25, No. 2, 1988, pp. 914-922.
33. Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Airfoil in Compressible Flight Speed Regimes Exposed to Blast Loadings," Aerospace Science and Technology, Vol. 6, No. 3, 2002, pp. 259-272.
34. Qin, Z., Marzocca, P., and Librescu, L., "Aeroelastic Instability and Response of Advanced Aircraft Wings at Subsonic Flight Speeds," Aerospace Science and Technology, Vol. 6, No. 5, 2002, pp. 195-208.
35. Krstić, M., Kanellakopoulos, I., and Kokotović, P., Nonlinear and Adaptive Control Design, Wiley, New York, 1995.
36. Kokotovic, P., "The Joy of Feedback: Nonlinear and Adaptive," Institute of Electrical and Electronic Engineers Control Systems Magazine, Vol. 12, June 1992, pp. 7-17.
37. Kim, J., and Crassidis, J. L., "Limit Cycle Oscillation Control of Aeroelastic Systems Using Model-Error Control Synthesis," AIAA Paper 2003-5506, Aug. 2003.
38. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Dover, New York, 1996, Chap. 6.