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Fault tolerant control for partial loss of control authority in aircraft using piecewise affine slab models

Title:

Fault tolerant control for partial loss of control authority in aircraft using piecewise affine slab models

Nayebpanah, Nastaran, Rodrigues, Luis and Zhang, Youmin (2013) Fault tolerant control for partial loss of control authority in aircraft using piecewise affine slab models. Journal of the Franklin Institute . ISSN 00160032 (In Press)

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Official URL: http://dx.doi.org/10.1016/j.jfranklin.2013.02.023

Abstract

In this paper, a new fault tolerant control methodology is proposed for partial loss of control authority in aircraft using piecewise affine (PWA) slab models while minimizing an upper bound on a quadratic cost function. The proposed controller stabilizes and satisfies performance bounds for both the nominal and faulty systems. The controller design criteria are cast as a set of Linear Matrix Inequalities (LMIs) that can be solved efficiently. The new technique is illustrated in a numerical example for the Beechcraft 99 aircraft model.

Divisions:Concordia University > Gina Cody School of Engineering and Computer Science > Electrical and Computer Engineering
Item Type:Article
Refereed:Yes
Authors:Nayebpanah, Nastaran and Rodrigues, Luis and Zhang, Youmin
Journal or Publication:Journal of the Franklin Institute
Date:2013
Digital Object Identifier (DOI):10.1016/j.jfranklin.2013.02.023
ID Code:977031
Deposited By: DANIELLE DENNIE
Deposited On:08 Apr 2013 14:21
Last Modified:18 Jan 2018 17:43

References:

1]P.R. Chandler, Self-repairing flight control system reliability and maintainability program? Executive overview, in: Proceedings of the IEEE National Aerospace and Electronics Conference, Dayton, OH, 1984, pp. 586–590.

[2] Y.M. Zhang, J. Jiang Bibliographical review on reconfigurable fault-tolerant control systems Annual Reviews in Control, 2 (2) (2008), pp. 229–252

[3]J.S. Eterno, J.L. Weiss, D.P. Looze, A.S. Willsky, Design issues for fault tolerant-restructurable aircraft control, in: 24th IEEE Conference on Decision and Control, December, 1985, pp. 900–905.

[4]X. Li, H.H.T. Liu. A passive fault tolerant flight control for maximum allowable vertical tail damaged aircraft. ASME Journal of Dynamic Systems, Measurement, and Control, 134 (May) (2012), pp. 031006-1–031006-15

[5]Y.M. Zhang, J. Jiang. Integrated active fault-tolerant control using IMM approach IEEE Transactions on Aerospace and Electronic Systems, 37 (4) (2001), pp. 1221–1235

[6] J. Jiang. Fault-tolerant control systems? An introductory overview Automatica SINCA, 31 (1) (2005), pp. 161–174

[7]R.J. Patton, Fault-tolerant control systems: the 1997 situation, in: Proceedings of the 3rd IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes, Hull, UK, August 1997, pp. 1033–1055.

[8]R.F. Stengel, Intelligent Failure-Tolerant Control IEEE Control Systems Magazine, 11 (4) (1991), pp. 14–23

[9]Y.M. Zhang, J. Jiang, Issues on integration of fault diagnosis and reconfigurable control in active fault-tolerant control systems, Reprints of the Sixth IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes, 2006, pp. 1513–1524.

[10]L. Rodrigues, S. Boyd Piecewise-affine state feedback for piecewise-affine slab systems using convex optimization Systems & Control Letters, 54 (9) (2005), pp. 835–853

[11]D. Liberzon, Switching in Systems and Control, Volume in series Systems and Control, Birkhauser, Boston, June 2003.

[12]J.H. Richter, W.P.M.H. Heemels, N. van de Wouw, J. Lunze, Reconfigurable control of PWA systems with actuator and sensor faults: stability, in: 47th IEEE Conference on Decision and Control, Cancun, Mexico, 2008, pp. 1060–1065.

[13]J. Lofberg, YALMIP: a toolbox for modeling and optimization in MATLAB, in: Proceedings of the CACSD Conference, Taipei, Taiwan, 2004, pp. 284–289.

[14]P. Stoddart, L. Rodrigues, Inverse optimal nonlinear control of a UAV on a longitudinal plane, in: Proceedings of the First European Guidance, Navigation and Control Conference, Munich, Germany, April 2011.

[15]N.E. Wu, Y.M. Zhang, K. Zhou. Detection, estimation, and accommodation of loss of control effectiveness. International Journal of Adaptive Control and Signal Processing, 14 (7) (2000), pp. 775–795

[16]Y.M. Zhang, J. Jiang. An active fault-tolerant control system against partial actuator failures. IEE Proceedings of Control Theory and Applications, 149 (1) (2002), pp. 95–104

[17]K. Zhou, P.K. Rachinayani, N. Liu, Z. Ren, J. Aravena, Fault diagnosis and reconfigurable control for flight control systems with actuator failures, in: 43rd IEEE Conference on Decision and Control, Bahamas, December 2004, pp. 5266–5271.

[18]L. Rodrigues, J. How, Automated control design for a piecewise-affine approximation of a class of nonlinear systems, in: Proceedings of the American Control Conference, Arlington, Virginia, 2001, pp. 3189–3194.

[19]A. Jadbabaie, M. Jamshidi, A. Titli, Guaranteed-cost design of continuous-time Takagi–Sugeno fuzzy controllers via linear matrix inequalities, in: IEEE World Congress on Computational Intelligence, Fuzzy Systems Proceedings, vol. 1, 1998, pp. 268–273.

[20]D.J. Choi, P. Park, Guaranteed cost LPV output-feedback controller design for nonlinear systems, in: Proceedings IEEE International Symposium on Industrial Electronics, vol. 2, 2001, pp. 1198–1203.

[21]M. Ellison, Optimal Linear Quadratic Control, Lecture Notes in Recursive Methods for Macroeconomics, The University of Warwick, UK, 2004.

[22]R.R. Tanner, T.D. Montgomery, Stability and control derivative estimates obtained from flight data for the Beech 99 Aircraft, NASA Technical Memorandum, April 1979.
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