Aircraft flight controls design using constrained output feedback: A H∞ loopshaping approach

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Kureemun, Ridwan ^a   Bates, Declan G ^a  

^a UNIVERSITY OF LEICESTER   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894427622     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Lewis, F. L., Optimal Control, Wiley, 1986.
2. Zhou, K., Doyle, J. C. and Glover, K., Robust and Optimal Control, Prentice Hall, 1996.
3. Skogestad, S. and Postlethwaite, I., "Multivariable Feedback Control", Wiley, 1998.
4. Stevens, B.L. and Lewis, F.L., "Aircraft Control and Simulation", Wiley, 1992.
5. Stevens, B. L., Vesty, P., Heck, B. S. and Lewis, F. L., "Loop Shaping with Output Feedback", Proceedings of the American Control Conference, pp. 146-149, 1987.
6. Stevens, B. L., Lewis, F. L. and Al-Sunni, F., "Aircraft Flight Controls Design using Output Feedback", AIAA Journal of Guidance, Control and Dynamics, 1991.
7. Boyd, S. P. and Barratt, C. H., Linear Controller Design-Limits of Performance, Prentice Hall, 1991.
8. Doyle, J. C., Packard, A., Zhou, K., "Review of LFTs, LMIs and //", Proc. 30th Conf. on Decision and Control, pp. 1227-1232, 1991.
9. Skelton, R. E., Stoustrup, J. and Iwasaki, T., "The Hoc Control Problem using Static Output Feedback", Int. Journal of Robust and Nonlinear Control, Vol. 4, pp. 449-455, 1994.
10. ∞ Control of Linear Systems with Time-Varying Uncertainties via Static Output Feedback", Proceedings of the Int. Mechanical Engineering Congress and Exposition, San Francisco, CA, 1995.
11. rd IEEE Conference on Decision and Control, Florida, 1994.
12. ∞ fixed-order controllers", International Journal of Robust and Nonlinear Control, 10, pp. 1237-1248, 2000.
13. Schmitendorf, W. E., "Output feedback control with configuration constraints on the gains", Proc. 14th Int. Conf. on Systems Engineering, UK, 2000.
14. McFarlane, D., and Glover, K., "A Loop Shaping Design Procedure using H^ Synthesis", IEEE Transactions on Automatic Control, AC-36, pp. 759-769, 1992.
15. ∞Aerospace Control Design-A VSTOL Flight Application, Springer Verlag, 1995.
16. Smerlas, A., Postlethwaite, I., Walker, D. J., Strange, M. E., Howitt, J., Horton, R. L, Gubbels, A. W. and Baillie, S. W., "Design and Flight Testing of an HQQ Controller for the NRC Bell 205 experiemntal Fly-By-Wire Helicopter", Proceedings of the AIAA Conference on Guidance, Navigation and Control, Boston, 1998.
17. Le Ballois, S. and Due, G., "Hoc Control of an Earth Observation Satelite", AIAA Journal of Guidance Navigation and Control, 19(3), pp. 628-635, 1996.
18. Bates, D. G., Gatley, S. L., Postlethwaite, I. and Berry, A. J., "Design and Piloted Simulation of a Robust Integrated Flight and Propulsion Controller", AIAA Journal of Guidance, Navigation and Control, 23(2), pp. 269-277, 2000.
19. Ferreres, G., and M'Saad, M., "Parametric Robustness Analysis of a Missile Autopilot", AIAA journal of Guidance Control and Dynamics, 19(3), pp. 621-627, 1996.
20. Samar, R., Robust Multi-Mode Control of High Performance Aero-Engines, Ph.D. Thesis, Department of Engineering, University of Leicester, UK, 1995.
21. ∞Loop Shaping: Why is it a Sensible Procedure for Designing Robust Flight Controllers?", in Proceedings of the AIAA Conference on Guidance, Navigation and Control, Oregon, AIAA-99-4272/3, 1999.
22. Glover, K., "All optimal Hankel-norm approximations of linear multivariable systems and their LOO error bounds", International Journal of Control, vol. 39, pp. 1115-1193, 1984.
23. Morton, B. and McAfoos, R., "A /x-test for real parameter variations", Proceedings of the American Control Conference, pp. 135-138, 1985.
24. Balas, G. J., Doyle, J. C., Glover, K., Packard, A. and Smith, R., μ-analysis and synthesis toolbox, The Math Works, 1995.