Longitudinal axis flight control law design by adaptive backstepping

IEEE Transactions on Aerospace and Electronic Systems

Volumn 43, Issue 1, 2007, Pages 311-329

  Ju, Hann Shing ^a   Tsai, Ching Chih ^a  

^a NATIONAL CHUNG HSING UNIVERSITY   (Taiwan)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; UNCERTAIN SYSTEMS;

ADAPTIVE BACKSTEPPING; SPECIFICATION ASSIGNMENTS;

FLIGHT CONTROL SYSTEMS;

EID: 34248669888     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2007.357136     Document Type: Article

References (30)

1. Watson, J. Fly-by-wire flight control system design considerations for the F-16 flight aircraft. Proceedings of the AIAA Guidance and Control Conference, 1976, AIAA-76-1915.
2. Shamma, J. S., and Athans, M. Analysis of gain scheduled control for nonlinear plants. IEEE Transactions on Automatic Control, 35 8 (1990), 898-907.
3. Gonsalves, P. G., and Zachariisa, G. L. Fuzzy logic gain scheduling for flight control. Proceedings of the IEEE Conference on Fuzzy Systems vol. 2, 1994, 952-957.
4. Wu, F. Z., Nikiforuk, P. N., and Gupta, M. M. A design of a flight control system using fuzzy gain-scheduling. Proceedings of AIAA Guidance Navigation and Control Conference, 1997, AIAA-97-3760.
5. Adams, R. J., and Banda, S. S. Robust flight control design using dynamic inversion and structured singular value synthesis. IEEE Transactions on Control Systems Technology, 1, 2 (1993), 80-92.
6. Bacon, B. J., Ostroff, A. J., and Joshi, S. M. Reconfigurable NDI controller using inertial sensor failure detection and isolation. IEEE Transactions on Aerospace and Electronic Systems, 37, 4 (2001), 1373-1383.
7. Lee, H. C., and Choi, J. W. Linear time-varying eigenstructure assignment with flight control application. IEEE Transactions on Aerospace and Electronic Systems, 40, 1 (2004), 145-157.
8. Singh, S. N., Steinberg, M., and Digirolamo, R. Variable structure robust flight control system for the F-14. IEEE Transactions on Aerospace and Electronic Systems, 33, 1 (1997), 77-84.
9. Lu, X. Y., Spurgeon, S. K., and Postlethwaite, I. Robust variable structure control of a PVTOL aircraft. International Journal of Systems Science, 28, 6 (1997), 547-558.
10. Jafarov, E. M., and Tasaltin, R. Robust sliding-mode control for the uncertain MIMO aircraft model F-18. IEEE Transactions on Aerospace and Electronic Systems, 36, 4 (2000), 1127-1141.
11. Harkegard, O., and Torkel Glad, T. A backstepping design for flight path angle control. Proceedings of the IEEE Conference on Decision and Control, vol. 4, 2000, 3570-3575.
12. Lee, T., and Kim, Y. Nonlinear adaptive flight control using backstepping and neural networks controller. AIAA Journal of Guidance, Control, and Dynamics, 24, 4 (2001), 675-682.
13. Sharma, M., and Ward, D. G. Flight-path angle control via neuro-adaptive backstepping. Proceedings of the AIAA Guidance, Navigation, and Control Conference, 2002, AIAA-2002-4451.
14. Sparks, A. G., Buffington, J. M., and Banda, S. S. Fighter aircraft lateral axis full envelope control law design. Proceedings of IEEE Conference on Control Applications, vol. 1, 1993, 21-26.
15. Reynolds, O. R., Pachter, M., and Houpis, C. H. Full envelope flight control system design using QFT. Proceedings of the American Control Conference, 1, 29 (1994), 350-354.
16. Blight, J. D., Gangsaas, D., and Richardson, T. M. Control law synthesis for an airplane with relaxed static stability. AIAA Journal of Guidance, Control, and Dynamics, 9, 5 (1986), 546-554.
17. Ju, H. S., Tsai, C. C., and Liu, S. W. Design of longitudinal axis full envelope control law by adaptive backstepping. Proceedings of the 2004 IEEE International Conference on Networking, Sensing and Control vol. 2, 2004, 755-760.
18. Roskam, J. Airplane Flight Dynamics & Automatic Flight Control. Lawrence, KA: Kansas University Press, 1979, 412-441.
19. Pratt, R. W., and Zarchan, P. Flight Control System. Reston, VA: AIAA, 2000, 1-20.
20. Sharma, M., and Calise, A. J. Adaptive backstepping control for a class of nonlinear systems via multilayered neural networks. Proceedings of the American Control Conference, vol. 4, May 2002, 2683-2688.
21. Dahlgren, J. Robust Nonlinear Control Design for a Missile Using Backstepping. Sweden: Linkoping University Electronic Press, 2002, 3-11.
22. Farrell, J., Sharma, M., and Polycarpou, M. On-line approximation based aircraft longitudinal control. Proceedings of the American Control Conference, vol. 2, 2003, 1011-1019.
23. Khail, H. K. Nonlinear System (2nd ed.). Englewwod Cliffs, NJ: Prentice-Hall, 1996, 588-601.
24. Kanellakopoulos, I., and Krein, P. T. Integral-action nonlinear control of induction motors. Proceedings of the 12th IFAC World Congress, 1993, 251-254.
25. Krstic, M., Kanellakopoulos, I., and Kokotovic P. Nonlinear and Adaptive Control Design. New York: Wiley, 1995, 87-99.
26. Mangold, P. Integration of Handling Quality Aspects into the Aerodynamic Design of Modern Unstable Fighters. AGARD Symposium on Flying Qualities, 1990.
27. MIL-F-8785C Military Specification, Flying Qualities of Pilot Airplane. Wright Patterson AFB, 1980, 13-21.
28. Phillips, S. N., Pachter, M., Houpis, C. H., and Rasmussen, S. J. A QFT subsonic envelope flight control system design. Aerospace and Electronics Conference, vol. 1, 1995, 537-544.
29. Siwakosit, W., Snell, S. A., and Hess, R. A. Robust flight control design with handling qualities constraints using scheduled linear dynamic inversion and loop shaping. IEEE Transactions on Control Systems Technology, 8 (2000), 483-494.
30. McLean, D. Automatic Flight Control Systems. Englewood Cliffs, NJ: Prentice-Hall, 1990, 199-206.