Control of a Nonlinear Wing Section Using Leading- and Trailing-Edge Surfaces

Journal of Guidance, Control, and Dynamics

Volumn 27, Issue 1, 2004, Pages 52-58

  Platanitis, George ^a,b   Strganac, Thomas W ^a,b  

^a TEXAS A AND M UNIVERSITY   (United States)

^b Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; ALGEBRA; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL EQUIPMENT; FEEDBACK CONTROL; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; STIFFNESS; WIND TUNNELS; WINGS;

INERTIA; LINEAR QUADRATIC REGULATOR (LQG); TRAILING EDGE CONTROL;

AERODYNAMICS;

EID: 1042275383     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.9284     Document Type: Article

References (19)

1. Rule, J. A., Richard, R. E., and Clark, R. L., "Design of an Aeroelastic Delta Wing Model for Active Flutter Control," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 919-924.
2. Wazak, M., and Srinathkumar, S., "Design and Experimental Validation of a Flutter Suppression Controller for the Active Flexible Wing," NASA TM 4381, Office of Management, Scientific and Technical Information Program, Washington, DC, 1992.
3. Mukhopadhyay, V., "Flutter Suppression Digital Control Law Design and Testing for the AFW Wind Tunnel Model," NASA TM 107652, Langley Research Center, Hampton, VA, 1992.
4. 2-Synthesis Controllers on an Experimental Typical Section," Journal of Guidance, Control, and Dynamics, Vol. 22, No. 2, 1999, pp. 278-285.
5. Denegri, C. M., Jr., and Johnson, M. R., "Limit-Cycle Oscillation Prediction Using Artificial Neural Networks," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 887-895.
6. Denegri, C. M., Jr., and Cutchins, M. A., "Evaluation of Classical Flutter Analysis for the Prediction of Limit Cycle Oscillations," AIAA Paper 97-1021, April 1997.
7. 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.
8. 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.
9. Ko, J., Strganac, T. W., and Kurdila, A. J., "Stability and Control of a Structurally Nonlinear Aeroelastic System," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 5, 1998, pp. 718-725.
10. 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.
11. 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. 503-509.
12. Ko, J., Strganac, T. W., and Kurdila, A. J., "Adaptive Feed-back Linearization for the Control of a Typical Wing Section With Structural Nonlinearity," Nonlinear Dynamics, Vol. 18, No. 3, 1999, pp. 289-301.
13. Strganac, T. W., Ko, J., and Thompson, D. E., "Identification and Control of Limit-Cycle Oscillations in Aeroelastic Systems," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 6, 2000, pp. 1127-1133.
14. Strganac, T. W., Ko, J., Thompson, D. E., and Kurdila, A. J., "Investigations of Limit Cycle Oscillations in Aeroelastic Systems," NASA CP-1999-209136, June 1999.
15. Kurdila, A., Strganac, T., Junkins, J., Ko, J., and Akella, M., "Nonlinear Control Methods for High-Energy Limit-Cycle Oscillations," Journal of Guidance, Control and Dynamics, Vol. 24, No. 1, 2001, pp. 185-192.
16. Thompson, D., "Nonlinear Analysis of Store-Induced Limit Cycle Oscillations.''M.S. Thesis, Dept. of Aerospace Engineering, Texas A&M Univ., College Station, TX, Aug. 2001.
17. Isidori, A., Nonlinear Control Systems, Springer-Verlag, New York, 1989, pp. 1-82.
18. Mukhopadhyay, V., "Transonic Flutter Suppression Control Law Design, Analysis, and Wind Tunnel Results," NASA CP-1999-209136/PT-1, June 1999.
19. La Salle, J., and Lefschetz, S., Stability by Liapunov's Direct Method, Academic Press, New York, 1961, pp. 37-73.