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Fault Detection and Fault-Tolerant Control Using Sliding Modes pp 271–290Cite as

SIMONA Implementation Results

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

Abstract

This chapter describes the implementation of the sliding mode allocation schemes from the previous chapter on the 6-DOF research flight simulator SIMONA at Delft University of Technology, the Netherlands. The controller is implemented in ‘C’ and runs on the ‘flight control’ computer associated with SIMONA. Real-time implementation issues are discussed and a range of fault scenarios from the GARTEUR AG16 benchmark are tested and discussed.

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Notes

  1. 1.

    Spoilers 6 and 7 are ground spoilers and are not used during flight [119].

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Author information

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

Authors
  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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Corresponding author

Correspondence to Halim Alwi .

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© 2011 Springer-Verlag London Limited

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Alwi, H., Edwards, C., Tan, C.P. (2011). SIMONA Implementation Results. 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_11

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  • DOI: https://doi.org/10.1007/978-0-85729-650-4_11

  • Publisher Name: Springer, London

  • Print ISBN: 978-0-85729-649-8

  • Online ISBN: 978-0-85729-650-4

  • eBook Packages: EngineeringEngineering (R0)

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