Abstract
In this chapter a quite different approach is adopted: here an integral sliding mode approach will be retro-fitted to an existing feedback controller. The fault tolerant control allocation scheme in this chapter adopts an a posteri approach, building on an existing state feedback controller designed using only the primary actuators.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Notes
References
Härkegård, O., Glad, S.T.: Resolving actuator redundancy—optimal control vs. control allocation. Automatica 41, 137–144 (2005)
Shin, D., Moon, G., Kim, Y.: Design of reconfigurable flight control system using adaptive sliding mode control: actuator fault. Proc. Inst. Mech. Eng. Part G: J. Aerosp. Eng. 219, 321–328 (2005)
Liu, G.P., Patton, R.J.: Eigenstructure Assignment for Control Systems Design. Wiley, Chichester (1998)
Ganguli, S., Marcos, A., Balas, G.J.: Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis. In: Proceedings of the American Control Conference (2002)
Duan, G.: Parametric eigenstructure assignment via output feedback based on singular value decompositions. IEE Control Theory Appl. 150(1), 93–100 (2003)
Hess, R.A., Wells, S.R.: Sliding mode control applied to reconfigurable flight control design. J. Guid. Control Dyn. 26, 452–462 (2003)
Shtessel, Y., Buffington, J., Banda, S.: Tailless aircraft flight control using multiple time scale re-configurable sliding modes. IEEE Trans. Control Syst. Technol. 10, 288–296 (2002)
Alwi, H., Edwards, C., Tan, C.P.: Fault Detection and Fault Tolerant Control Using Sliding Modes. Advances in Industrial Control Series. Springer, Berlin (2011)
Wohletz, J.M.: Retrofit Systems for Reconfiguration in Civil Aviation. PhD thesis, MIT (2000)
Doyle, M.E.: Retrofit reconfigurable flight control system and the F/A-18C. Master’s thesis, University of Tennessee - Knoxville (2006)
Bošković, J.D., Bergstrom, S.E., Mehra, R.K.: Retrofit reconfigurable flight control in the presence of control effector damage. In: Proceedings of the American Control Conference, pp. 2652–2657 (2005)
Bošković, J.D., Prasanth, R., Mehra, R.K.: Retrofit fault-tolerant flight control design under control effector damage. J. Guid. Control Dyn. 30(3), 703–712 (2007)
Bošković, J.D.: A new decentralized retrofit adaptive fault-tolerant flight control design. In: International Journal of Adaptive control and signal Processing (2012)
Farineau, J.: Lateral electric flight control laws of a civil aircraft based upon eigenstructure assignment technique. In: American Institute of Aeronautics and Astronautics (1989)
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2016 Springer International Publishing Switzerland
About this chapter
Cite this chapter
Hamayun, M.T., Edwards, C., Alwi, H. (2016). An Augmentation Scheme for Fault Tolerant Control Using Integral Sliding Modes. In: Fault Tolerant Control Schemes Using Integral Sliding Modes. Studies in Systems, Decision and Control, vol 61. Springer, Cham. https://doi.org/10.1007/978-3-319-32238-4_6
Download citation
DOI: https://doi.org/10.1007/978-3-319-32238-4_6
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-32236-0
Online ISBN: 978-3-319-32238-4
eBook Packages: EngineeringEngineering (R0)