Fault tolerant control of a civil aircraft using a sliding mode based scheme

Proceedings of the 44th IEEE Conference on Decision and Control, and the European Control Conference, CDC-ECC '05

Volumn 2005, Issue , 2005, Pages 1011-1016

  Alwi, Halim ^a   Edwards, Christopher ^a  

^a UNIVERSITY OF LEICESTER   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CONTROL EQUIPMENT; FAULT TOLERANT COMPUTER SYSTEMS; SWITCHING; VECTORS;

FAULT TOLERANT CONTROL; FLIGHT ENVELOPE; RECONFIGURABLE CONTROL; SWITCHING VARIABLES;

SLIDING MODE CONTROL;

EID: 33847181277     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/CDC.2005.1582290     Document Type: Conference Paper

References (17)

1. Boyd S.P., El Ghaoui L., Feron E., Balakrishnan V., Linear Matrix Inequalities in Systems and Control Theory, SIAM, 1994.
2. Edwards C and Spurgeon S.K., Sliding Mode Control: Theory and Applications. Taylor & Francis, 1998.
3. Ganguli S, Marcos A, Balas G.J, "Reconfigurable LPV Control Design for Boeing 747-100/200 Longitudinal Axis", American Control Conference, Anchorage, Alaska, May 2002;
4. Hess R.A, Wells S.R. "Sliding mode control applied to reconfigurable flight control design" Journal of Guidance, Control, and Dynamics, v 26, n 3, May-June 2003, p 452-62
5. Huzmezan M and Maciejowski J, "Reconfigurable Flight Control Methods and Related Issues - A Survey" Technical report prepared for the DERA under the Research Agreement no. ASF/3455, Department of Engineering, University of Cambridge, August 1997.
6. Khalil H.K., Nonlinear Systems, Prentice Hall, Englewood Cliffs NJ., 1992.
7. Marcos A, Balas G.J, "A Boeing 747-100/200 Aircraft Fault Tolerant and Fault Diagnostic Benchmark", Technical report AEM-UoM-2003-1, Department of Aerospace and Engineering mechanics, University of Minnesota, USA, June, 2003.
8. Maciejowski J.M., Jones C N. "MPC Fault-Tolerant Control Case Study: Flight 1862", SAFEPROCESS 03, Washington, 2003.
9. Patton R.J, 'Robustness in model-based fault diagnosis: the 1997 situation,' IFAC Annual Reviews, vol. 21, pp. 101-121, 1997.
10. Shtessel Y, Buffington J, Banda S, "Multiple timescale flight control using reconfigurable sliding modes ", Journal of Guidance, Control, and Dynamics, v 22, n 6, Nov-Dec, 1999, p 873-883
11. Smaili M.H "FLIGHTLAB 747: Benchmark for Advance Flight Control Engineering", technical report, Technical University Delft, The Netherlands, 1999
12. Ryan E.P and Corless M., "Ultimate boundedness and asymptotic stability of a class of uncertain dynamical systems via continuous and discontinuous control", IMA Journal of Mathematical Control and Information, v 1, 1984, p 223-242.
13. Utkin V.I., Sliding Modes in Control Optimization, Springer-Verlag, Berlin, 1992.
14. van der Linden C.A.A.M. "DASMAT: Delft University Aircraft, Simulation Model and Analysis Tool", Technical Report, LR-781 Technical University Delft, The Netherlands, 1996.
15. Wheeler G., Su C., Stepanenko Y., A sliding mode controller with improved adaptation laws for the upper bounds on the norm of uncertainties, Automatica, vol 34, 1657-1661, 1998.
16. Zhang Y, Jiang J. in "Bibliographical Review on Reconfigurable Fault Tolerant Control Systems", Proceedings of the IFAC Symposium SAFEPROCESS 03, Washington, 2003, pp. 265-276.
17. Zhou K, Rachinayani P.K, Liu N, Ren Z, Aravena J. "Fault Diagnosis and Reconfigurable Control for Flight Control System with Actuator Failures", 43rd IEEE Conf on Decision and Control, December 14-17, 2004, Atlantis, Paradise Island, Bahamas