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2015 | 25 | 1 | 93-102
Tytuł artykułu

A fault tolerant direct control allocation scheme with integral sliding modes

Treść / Zawartość
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In this paper, integral sliding mode control ideas are combined with direct control allocation in order to create a fault tolerant control scheme. Traditional integral sliding mode control can directly handle actuator faults; however, it cannot do so with actuator failures. Therefore, a mechanism needs to be adopted to distribute the control effort amongst the remaining functioning actuators in cases of faults or failures, so that an acceptable level of closed-loop performance can be retained. This paper considers the possibility of introducing fault tolerance even if fault or failure information is not provided to the control strategy. To demonstrate the efficacy of the proposed scheme, a high fidelity nonlinear model of a large civil aircraft is considered in the simulations in the presence of wind, gusts and sensor noise.
Rocznik
Tom
25
Numer
1
Strony
93-102
Opis fizyczny
Daty
wydano
2015
otrzymano
2014-01-30
poprawiono
2014-06-18
Twórcy
  • Department of Electrical Engineering, COMSATS Institute of Information Technology, Lahore, Pakistan
  • Department of Engineering, College of Engineering, Mathematics and Physical Sciences, University of Exeter, UK
autor
  • Department of Engineering, College of Engineering, Mathematics and Physical Sciences, University of Exeter, UK
  • Department of Aeronautical Engineering, King Abdul Aziz University, Jeddah, Saudi Arabia
Bibliografia
  • Alwi, H. and Edwards, C. (2008a). Fault tolerant control using sliding modes with on-line control allocation, Automatica 44(7): 1859-1866.
  • Alwi, H. and Edwards, C. (2008b). Fault tolerant sliding mode control design with piloted simulator evaluation, Journal of Guidance, Control, and Dynamics 31(5): 1186-1201.
  • Alwi, H., Edwards, C. and Tan, C. (2011). Fault Detection and Fault Tolerant Control Using Sliding Modes, Advances in Industrial Control, Springer-Verlag, London.
  • Bošković, J. and Mehra, R. (2002). Control allocation in overactuated aircraft under position and rate limiting, American Control Conference, Anchorage, AK, USA, pp. 791-796.
  • Boyd, S., Ghaoui, L., Feron, E. and Balakrishnan, V. (1994). Linear Matrix Inequalities in System and Control Theory, SIAM, Philadelphia, PA.
  • Castaldi, P., Mimmo, N. and Simani, S. (2011). Fault tolerant control schemes for nonlinear models of aircraft and spacecraft systems, 18th IFAC World Congress, Milan, Italy, pp. 13705-13710.
  • Castaldi, P., Mimmo, N. and Simani, S. (2014). Differential geometry based active fault tolerant control for aircraft, Control Engineering Practice 32: 227-235, DOI: 10.1016/j.conengprac.2013.12.011i.
  • Davidson, J., Lallman, F. and Bundick, W. (2001). Real-time adaptive control allocation applied to a high performance aircraft, 5th SIAM Conference on Control and Its Application, Hampton, VA, USA, pp. 1-1.
  • Ducard, G.J.J. (2009). Fault-tolerant Flight Control and Guidance Systems: Practical Methods for Small Unmanned Aerial Vehicles, Advances in Industrial Control, Springer-Verlag, London.
  • Edwards, C., Alwi, H. and Tan, C.P. (2012). Sliding mode methods for fault detection and fault tolerant control with application to aerospace systems, International Journal of Applied Mathematics and Computer Science 22(1): 109-124, DOI: 10.2478/v10006-012-0008-7.
  • Edwards, C., Lombaerts, T. and Smaili, H. (2010). Fault Tolerant Flight Control: A Benchmark Challenge, Lecture Notes in Control and Information Sciences, Vol. 399, Springer-Verlag, Berlin/Heidelberg.
  • Edwards, C. and Spurgeon, S. (1998). Sliding Mode Control, Theory and Applications, Taylor and Francis, London.
  • Hamayun, M. (2013). Integral Sliding Mode Fault Tolerant Control Schemes with Control Allocation, Ph.D. thesis, University of Leicester, Leicester.
  • Hamayun, M., Edwards, C. and Alwi, H. (2012). Design and analysis of an integral sliding mode fault tolerant control scheme, IEEE Transactions on Automatic Control 57(7): 1783-1789.
  • Hamayun, M., Edwards, C. and Alwi, H. (2013). An output integral sliding mode FTC scheme using control allocation, Automatica 49(6): 1830-1837.
  • Harkegard, O. and Glad, S. (2005). Resolving actuator redundancy-optimal vs. control allocation, Automatica 41(1): 137-144.
  • Hess, R. and Wells., S. (2003). Sliding mode control applied to reconfigurable flight control design, Journal of Guidance, Control and Dynamics 26(3): 452-462.
  • Johansen, T. and Fossen, T.I. (2013). Control allocation-a survey, Automatica 49(5): 1087-1103.
  • Khalil, H. (1992). Nonlinear Systems, Prentice Hall, Englewood Cliffs, NJ.
  • Marcos, A. and Balas, G. (2003). A Boeing 747-100/200 aircraft fault tolerant and diagnostic benchmark, Technical report, Department of Aerospace and Engineering Mechanics, University of Minnesota, Minneapolis, MN.
  • Ogata, K. (2002). Modern Control Engineering, 4th Edn., Prentice Hall, London.
  • Shtessel, Y., Buffington, J. and Banda, S. (2002). Tailless aircraft flight control using multiple time scale re-configurable sliding modes, IEEE Transactions on Control Systems Technology 10(2): 288-296.
  • Utkin, V., Guldner, J. and Shi, J. (1999). Sliding Mode Control in Electromechanical Systems, Taylor and Francis, London.
  • Utkin, V. and Shi, J. (1996). Integral sliding mode in systems operating under uncertainty conditions, 35th IEEE Conference on Decision and Control, Kobe, Japan, pp. 4591-4596.
  • Verhaegen, M., Kanev, S., Hallouzi, R., Jones, C., Maciejowski, J. and Smail, H. (2010). Fault tolerant flight control-a survey, in C. Edwards, T. Lombaerts and H. Smaili (Eds.), Fault Tolerant Flight Control, Lecture Notes in Computer Science, Vol. 399, Springer, Berlin/Heidelberg, pp. 47-89.
  • Wells, S. and Hess, R. (2003). Multi-input/multi-output sliding mode control for a tailless fighter aircraft, Journal of Guidance, Control, and Dynamics 26(3): 463-473.
  • Wu, N., Zhang, Y. and Zhou, K. (2000). Detection, estimation, and accommodation of loss of control effectiveness, International Journal of Adaptive Control and Signal Processing 14: 775-795.
  • Zhang, Y. and Jiang, J. (2003). Fault tolerant control system design with explicit consideration of performance degradation, IEEE Transactions on Aerospace and Electronic Systems 39(3): 838-848.
  • Zhang, Y. and Jiang, J. (2008). Bibliographical review on reconfigurable fault-tolerant control systems, Annual Reviews in Control 32(2): 229-252.
Typ dokumentu
Bibliografia
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