Abstract
This chapter describes an adaptive model reference sliding mode fault tolerant control scheme with online control allocation. As in the previous chapter, the control allocation scheme uses the effectiveness level of the actuators to redistribute the control signals to the remaining actuators when a fault or failure occurs. Meanwhile, the adaptive non-linear gain and reference model provide online tuning for the controller. This chapter provides a rigorous stability analysis for the model reference scheme. The scheme has been tested on a linearisation of the ADMIRE aircraft model to convey the ideas associated with the proposed scheme and shows that various faults and even total actuator failures can be handled.
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Alwi, H., Edwards, C., Tan, C.P. (2011). Model-Reference Sliding Mode FTC. In: Fault Detection and Fault-Tolerant Control Using Sliding Modes. Advances in Industrial Control. Springer, London. https://doi.org/10.1007/978-0-85729-650-4_10
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DOI: https://doi.org/10.1007/978-0-85729-650-4_10
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