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Fault Detection and Fault-Tolerant Control Using Sliding Modes

Part of the book series: Advances in Industrial Control ((AIC))

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Abstract

This chapter gives an overview of the recent developments in the area of fault detection and fault tolerance control. It is intended to provide motivation for the theoretical developments which follow in the subsequent chapters.

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Notes

  1. 1.

    Flight 232 suffered tail engine failure causing total loss of hydraulics [41, 109].

  2. 2.

    The freighter shed engine No. 1, but the crew managed to land safely.

  3. 3.

    The A300B4 was hit by a missile and lost all hydraulics, but landed safely [41].

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Authors and Affiliations

  1. Department of Engineering, University of Leicester, University Road, LE1 7RH, Leicester, UK

    Dr. Halim Alwi & Prof. Christopher Edwards

  2. School of Engineering, Monash University Sunway Campus, Jalan Lagoon Selatan, Bandar Sunway, 46150, Selangor, Malaysia

    Dr. Chee Pin Tan

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  1. Dr. Halim Alwi
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  2. Prof. Christopher Edwards
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  3. Dr. Chee Pin Tan
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Correspondence to Halim Alwi .

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Alwi, H., Edwards, C., Tan, C.P. (2011). Introduction. 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_1

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  • DOI: https://doi.org/10.1007/978-0-85729-650-4_1

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