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Model Reference Sliding Mode FTC with SIMONA Simulator Evaluation: EL AL Flight 1862 Bijlmermeer Incident Scenario

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Part of the book series: Lecture Notes in Control and Information Sciences ((LNCIS,volume 399))

Introduction

This chapter presents flight simulator results obtained by experienced pilots based on the EL AL flight 1862 (Bijlmermeer incident) scenario. The results in this chapter are the outcome of a controller evaluation ‘flight testing’ campaign and the GARTEUR AG16 final workshop at Delft University in November 2007. The results represent the successful real time implementation of a SMC controller in real time on the SIMONA 6-DOF flight simulator.

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References

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Alwi, H., Edwards, C., Stroosma, O., Mulder, J.A.(. (2010). Model Reference Sliding Mode FTC with SIMONA Simulator Evaluation: EL AL Flight 1862 Bijlmermeer Incident Scenario. In: Edwards, C., Lombaerts, T., Smaili, H. (eds) Fault Tolerant Flight Control. Lecture Notes in Control and Information Sciences, vol 399. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-11690-2_18

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  • DOI: https://doi.org/10.1007/978-3-642-11690-2_18

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-11689-6

  • Online ISBN: 978-3-642-11690-2

  • eBook Packages: EngineeringEngineering (R0)

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