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Fault Detection and Fault-Tolerant Control Using Sliding Modes pp 7–27Cite as

Fault Tolerant Control and Fault Detection and Isolation

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

Abstract

This chapter formally provides a definition of the terms fault and failure and briefly discusses the different types of faults and failures which can occur in actuators and sensors—with specific aircraft examples. The chapter introduces the concept of fault tolerant control and gives a general overview of the different FTC and FDI research fields. The main concepts and strategies behind some of the FTC and FDI schemes in the literature are also discussed.

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Notes

  1. 1.

    A blowdown limit is an aerodynamic limit of the control surface deflection at a specified speed which overpowers the movement of the actuator. The blowdown limits might not be the maximum physical deflection of the control surface. Any deflection above the blowdown limit can cause structural damage [240] as it imposes the maximum physical and structural limit the control surface and the surrounding structure can have.

  2. 2.

    Sensors, most of the time, provide measurements in terms of current or voltage and therefore require transformation to represent the actual physical meaning of the quantities being measured.

  3. 3.

    In terms of linear methods, system faults are the ones that affect the A matrix i.e., airframe or wing damage.

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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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Alwi, H., Edwards, C., Tan, C.P. (2011). Fault Tolerant Control and Fault Detection and Isolation. 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_2

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