H-infinity static output-feedback control for rotorcraft

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006

Volumn 3, Issue , 2006, Pages 1839-1850

  Gadewadikar, J ^a   Lewis, F L ^a   Subbarao, Kamesh ^b,d,e   Peng, Kemao ^c   Chen, Ben ^c  

^a UNIVERSITY OF TEXAS AT ARLINGTON   (United States)

^b University of Texas at Arlington   (United States)

^c NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

^d Box 19018 ^*  (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR CUSHION VEHICLES; ALGORITHMS; FEEDBACK CONTROL; LINEAR SYSTEMS; PROBLEM SOLVING; STABILIZATION;

CONTROL LAW; LINEAR TIME INVARIANT SYSTEMS; OUTPUT FEEDBACK CONTROL; ROTORCRAFT;

HELICOPTER ROTORS;

EID: 33845721779     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-6238     Document Type: Conference Paper

References (30)

1. Nakwan Kim, Anthony J. Calise, J. Eric Corban, and J.V.R. Prasad. "Adaptive Output Feedback for Altitude Control of an Unmanned Helicopter Using Rotor RPM". In AIAA Guidance, Navigation and Control Conference, August 2004
2. Eric N. Johnson and Suresh K. Kannan. "Adaptive Trajectory Control for Autonomous Helicopters". AIAA Journal of Guidance, Control, and Dynamics, 28(3), May-June 2005
3. Linda Wills, Suresh K. Kannan, Sam Sander, Murat Guler, Bonnie Heck, J.V.R Prasad, Daniel P. Schrage, and George Vachtsevanos. An Open Platform for Reconfigurable Control. In Tariq Samad and Gary J. Balas, editors,Software- Enabled Control: Information Technology for Dynamical Systems. IEEE Press, 2001.
4. Wayne Johnson, "Helicopter Theory", Dover Publications, Mineola, N. Y.
5. nd ed, Wiley Interscience, New York, 2003, pp 403-419.
6. Kim, Y. H., and Lewis F. L., High-Level Feedback Control with Neural Networks, World Scientific, Singapore, 1998, pp 55-75.
7. rd IEEE Conference on Decision and Control, Orlando, FL, 1994, pp. 837-842
8. nd ed, John Wiely and Sons, New York, 1995, pp. 359-375.
9. Moerder, D. D., and Calise, A. J., "Convergence of a Numerical Algorithm for calculating Optimal output feedback gains," IEEE Transactions on Automatic Control, Vol. 30, No. 9, 1985, pp. 900, 903.
10. Trofino-Neto, A., and Kucera, V., "Stabilization via static output feedback," IEEE Transactions on Automatic Control, Vol. 38, No. 5, 1993, pp. 764, 765.
11. Kucera, V., and De Souza, C. E., "A necessary and sufficient condition for output feedback stabilizability," IFAC Journal, AUTOMATICA, Vol. 31, No. 9, 1995, pp. 1357, 1359.
12. Geromel, J. C., and Peres, P. L.D., "Decentralized load-frequency control," IEE Proceedings, Vol. 132, Pt. D, No. 5, 1985, pp. 225, 230.
13. El Ghaoui, L., Oustry, F., AitRami, M., "A cone complementarity linearization algorithm for static output-feedback and related problems," IEEE Transactions on Automatic Control, Vol. 42, No. 8, 1997, pp. 1171-1176.
14. Geromel, J.C., de Souza, C.C.; and Skelton, R.E., "Static output feedback controllers: stability and convexity," IEEE Transactions on Automatic Control, Vol. 43, No. 1, 1998, pp. 120-125.
15. Cao, Y., Lam, J., and Sun, Y., "Static Output Feedback Stabilization: An ILMI approach," IFAC Journal, AUTOMATICA, Vol. 34, No. 12, 1998, pp. 1641-1645.
16. Gahinet, P., Nemirovski, A., Laub, A., and Chilali, M., LMI Control Tool box, MATLAB., Mathworks, Inc., Natick, MA, 1995.
17. Zames, G., "Feedback and optimal sensitivity: Model reference transformations, multiplicative seminoirms, and approximate inverses," IEEE Transactions on Automatic Control, Vol. 26, No. 2, 1981, pp. 301-320.
18. ∞ Control Problems," IEEE Transactions on Automatic Control, Vol. 34, No. 8, 1989, pp. 831-847.
19. ∞ Optimal Control and Related Minimax Design Problems, Berlin, Germany, Birkhauser, 1991, pp 4-6, 33-48.
20. Knobloch, H. W., Isidori, A., and Flockerzi, D., Topics in control theory, Birkhauser, Berlin, Germany, 1993, pp. 43-49, 58-67, 99-111.
21. ∞ viewpoint, Academic Press Interscience, San Diego, 1997, pp. 87-261.
22. rd IEEE Conference on Decision and Control, Atlantis, Paradise Island, Bahmas, 2004, pp. 3147-3153.
23. rd IEEE Conference on Decision and Control, Atlantis, Paradise Island, Bahmas, 2004, pp. 1188-1195.
24. Smerlas A.J., Walker D.J., Postlethwaite I., Strange M.E., Howitt J., Gubbels A.W., "Evaluating. H∞ controllers on the NRC Bell 205 fly-by-wire helicopter," Control Engineering Practice, 9(1), 2001, pp. 1-10.
25. Gadewadikar J, Lewis F., Abu-Khalaf M., "Necessary and Sufficient Conditions for H-∞ Static Output-Feedback Control," Journal of Guidance, Control, and Dynamics, Vol. 29, No. 4, July-August 2006, pp. 915-920.
26. ∞ Static State-Feedback Gains: Application to Output-Feedback Design," Automatica, in review,
27. ∞ Control," Springer, Berlin, 2000.
28. Klienman, D. L., "On an Iterative Technique for Riccati Equations Computations," IEEE Transactions on Automatic Control, Vol. 13, Issue 1. 1968, pp. 114-115.
29. Chen B., "Fourth Half Yearly Progress Report for the TYIA 2003 Project on Nonlinear Control Methods for Flight Control Systems of Flying Vehicles,DSTA, NUS, and ST AEROSPACE, Nov. 2005.
30. Hall Jr. W.E., and Bryson Jr. A.E., "The inclusion of rotor dynamics in controller design for helicopters," J. Aircraft, Vol 10, No 4., pp. 200-206.