Adaptive output feedback control of a nonlinear aeroelastic structure

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 6, 2000, Pages 1109-1116

  Xing, WenHong ^a   Singh, Sahjendra N ^a  

^a UNIVERSITY OF NEVADA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; ANGLE MEASUREMENT; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; EQUATIONS OF MOTION; FEEDBACK CONTROL; NONLINEAR CONTROL SYSTEMS; VECTORS; WINGS;

AEROELASTIC SYSTEM; BACKSTEPPING DESIGN TECHNIQUE; PITCH ANGLE MEASUREMENTS; PLUNGE DISPLACEMENT;

AERODYNAMICS;

EID: 0034314450     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4662     Document Type: Article

References (22)

1. Fung, Y. C., An Introduction to the Theory of Aeroelasticity, Wiley, New York, 1955, pp. 207-215.
2. Dowell, E. H., (ed.), A Modern Course in Aeroelasticity, Kluwer Academic, Norwell, MA, 1995, Chap. 1.
3. Zhao, L. C., and Yang, Z. C., "Chaotic Motions of an Airfoil with Nonlinear Stiffness in Incompressible Flow," Journal of Sound and Vibration, Vol. 128, No. 2, 1990, pp. 245-254.
4. Lyons, M. G., Vepa, R., McIntosh, I. E., and DeBra, D. B., "Control Law Synthesis and Sensor Design for Active Flutter Suppression," Proceedings of the AIAA Guidance and Control Conference, AIAA Paper 73-832, AIAA, New York, Aug. 1973.
5. Mukhopadhyay, V., Newsom, J. R., and Abel, I., "Reduced-Order Optimal Feedback Control Law Synthesis for Flutter Suppression," Journal of Guidance, Control, and Dynamics, Vol. 5, No. 4, 1982, pp. 389-395.
6. Gangsaas, D., Ly, U., and Norman, D. C., "Practical Gust Load Alleviation and Flutter Suppression Control Laws Based on LQG Methodology," AIAA Paper 81-0021, Jan. 1981.
7. Karpel, M., "Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling," Journal of Aircraft, Vol. 19, No. 3, 1982, pp. 221-227.
8. Edwards, J. W., Ashley, H., and Breakwell, J., "Unsteady Aerodynamic Modeling for Arbitrary Motions," AIAA Journal, Vol. 17, No. 4, 1979, pp. 365-374.
9. Horikawa, H., and Dowell, E. H., "An Elementary Explanation of the Flutter Mechanism with Active Feedback Controls," Journal of Aircraft, Vol. 16, No. 4, 1979, pp. 225-232.
10. Heeg, J., "Analytical and Experimental Investigation of Flutter Suppression by Piezoelectric Actuation," NASA TP 3241, Sept. 1993.
11. Lazarus, K., Crawey, 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.
12. Friedmann, P. 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.
13. Waszak, M. R., "Robust Multivariable Flutter Suppression for the Benchmark Active Control Technology (BACT) Wind-Tunnel Model," 11th Symposium on Structure Dynamics and Control, Blacksburg, VA, May 1997.
14. Tang, D. M., and Dowell, E. H., "Flutter and Stall Response of a Helicopter Blade with Structural Nonlinearity," Journal of Aircraft, Vol. 29, No. 5, 1990, pp. 953-960.
15. Lee, B. H. K., and LeBlanc, P., "Flutter Analysis of a Two-Dimensional Airfoil with Cubic Nonlinear Restoring Force," National Aeronautical Establishment, Aeronautical Note 36, Canada National Research Council 25438, Ottawa, PQ, Canada, Feb. 1986.
16. O'Neil, T., Gilliatt, H. C., and Strganac, T. W., "Investigations of Aeroelastic Response for a System with Continuous Structural Nonlinearities," AIAA Paper 96-1390, April 1996.
17. 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.
18. Ko, J., and Strganac, T. W., "Stability and Control of a Structurally Nonlinear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 5, 1998, pp. 718-725.
19. Block, J., and Strganac, T. M., "Applied Active Control for a Nonlinear Aeroelastic Structure," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 838-845.
20. Zeng, Y., and Singh, S. N., "Output Feedback Variable Structure Adaptive Control of an Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6, 1998, pp. 830-837.
21. Kanellakopoulos, I., and Kokotovic, P. V., and Morse, A. S., "Systematic Design of Adaptive Controller for Feedback Linearizable Systems," IEEE Transaction on Automatic Control, Vol. 36, No. 11, 1991, pp. 1241-1253.
22. Krstic, M., Kanellakopoulos, I., and Kokotovic, P. V., Nonlinear Adaptive Control Design, Wiley, New York, 1995, pp. 24, 25, 327-346.