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Case Study: ELAL Bijlmermeer Incident

  • Halim Alwi
  • Christopher Edwards
  • Chee Pin Tan
Part of the Advances in Industrial Control book series (AIC)

Abstract

This chapters presents the ELAL flight 1862 (Bijlmermeer incident) scenario—which is one of the case studies of GARTEUR AG16. The results presented in this chapter demonstrate the outcome of the ‘flight testing’ campaign and the GARTEUR AG16 final workshop at Delft University of Technology in November 2007. The results represent the successful real–time implementation of a sliding mode controller on SIMONA with experienced test pilots flying and evaluating the controller.

Keywords

Side Slip Angle Classical Controller Level Flight Flight Crew Flight Path Angle 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer-Verlag London Limited 2011

Authors and Affiliations

  • Halim Alwi
    • 1
  • Christopher Edwards
    • 1
  • Chee Pin Tan
    • 2
  1. 1.Department of EngineeringUniversity of LeicesterLeicesterUK
  2. 2.School of EngineeringMonash University Sunway CampusBandar SunwayMalaysia

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