Fault Tolerant Control With Re-Configuring Sliding-Mode Schemes

In this paper, a controller design method for linear MIMO systems is presented which a sliding mode controller is reconfigured in case of system faults. Faults are detected with the residual vector generated from a standard linear observer. Once a fault has been detected the fault distribution matrix can be obtained and used to update the corrective or equivalent control parts of the sliding mode controller. As a result, fault tolerant adaptive controllers keep the system performance within acceptable limits or at least avoids the system to wind-up.

Anahtar Kelimeler:

Fault detection, fault-tolerant systems, sliding-mode control, adaptive control, MIMO linear systems

Fault Tolerant Control With Re-Configuring Sliding-Mode Schemes

Keywords:

Fault detection, fault-tolerant systems, sliding-mode control, adaptive control, MIMO linear systems,

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H. E. Rauch, Intelligent Fault Diagnosis and Control Reconfiguration, IEEE Control Syst. Mag., June 1994.
M. Huzmezan, Reconfigurable Flight Control Methods and Related Issues, A Survey, DERA Report No: ASF/3455, Sep. 1997.
M. Huzmezan and J.M. Maciejowski, Automatic Tuning for Model Based Predictive Control During Reconfig- uration, in Proceedings of 14thIFAC Symposium on Automatic Control in Aerospace, Korea, August 1998.
H.E. Rauch, Autonomous Control Reconfiguration, IEEE Control Syst. Mag., Dec. 1995.
Z. Yang and M. Blanke, The Robust Control Mixer Module Method for Control Reconfiguration, in Proceedings of American Control Conference, June 2000.
D.D. Moerder, N.Halyo, J.R. Broussard, and A.K. Caglayan, Applications Of Pre-Computed Control Laws In A Reconfigurable Aircraft Flight Control System, Journal of Guidance, Control and Dynamics, 13(6), 1990.
P.S. Maybeck and R.D. Stevens, Reconfigurable Flight Control via Multiple Adaptive Control Methods, IEEE Transactions on Aerospace and Electronic Systems, 27(3), 1991.
Y. Ochi and K. Kanai, Design of Reconstructable Flight Control Systems Using Feedback Linearisation, Journal of Guidance, Control and Dynamics, 14(5), Sep.-Oct. 1991.
W.D. Morse and K.A. Ossman, Model Following Reconfigurable Flight Control System for the AFTI/F-16, Journal of Guidance, Control and Dynamics, 13(6), 1990.
J.J. Burke, P. Lu and Z. Wu, Reconfigurable Flight Control Designs with Application to the X-33 Vehicle, NASA Report No: TM-1999-206582, Aug. 1999.
A.P.Buckley, Hubble Space Telescope Pointing Control System Design Improvement Study Results, Journal of Guidance, Control and Dynamics, Mar.-Apr. 1995.
J.W. Sullivan, P. McCarty, G. Yoshimoto, R. Gargan and R. Pelavin, Intelligent System for Autonomous UUV Monitoring, Diagnosis and Control, Proceedings of 1992 AIAA Guidance, Navigation and Control Conf., Aug
J.Y. Hung, G. Weibing and J.C. Hung., Variable Structure Control: A Survey, IEEE Transactions on Industrial Electronics, Vol. 40, No.1, 1993.
V.I. Utkin, Variable Structure Systems with Sliding Modes, IEEE Transactions on Automatic Control, ACC- 2, 1977.
K.D. Young (Ed.), Variable Structure Control For Robotics And Aerospace Applications, New York: Elsevier- Science Publishers, 1993.
S.W. Wijesoma, Robust Trajectory Following of Robots Using Computed Torque Structure with VSS, Interna- tional Journal of Control, Vol.52, No.4, 1990.
Chen, J., and R. J. Patton, Robust Model-Based Fault Diagnosis for Dynamic Systems, Kluver A cademic Publishers, 1999.
Slotine, J. E., and W. P. Li, Applied Nonlinear Control, Prentice-Hall, 1991.
Patton, R. J., “Fault-Tolerant Control Systems: The 1997 Situation,” Proceedings SAFEPROCESS 97, Hull, UK, pp. 1033-1054, 1997.
Demirci, U., and F. Kerestecio˘glu, “Fault-Tolerant Reconfiguring Sliding Mode Controller”, Proc. ELECO 03 Conference, Bursa, pp. 279-283, 2003.