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SIMONA Implementation Results

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

Keywords

Control Surface Slide Mode Controller Switching Function Sideslip Angle Flight Simulator 
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.

References

  1. 35.
    Brière, D., Traverse, P.: Airbus A320/A330/A340 electrical flight controls: A family of fault-tolerant systems. Digest of papers FTCS-23 the twenty-third International Symposium on Fault-Tolerant Computing, Toulouse, France, pp. 616–623 (1993) Google Scholar
  2. 36.
    Bryson, A.E.: Control of Spacecraft and Aircraft. Princeton University Press, Princeton (1994) Google Scholar
  3. 43.
    Burcham, F.W., Maine, T.A., Kaneshinge, J., Bull, J.: Simulator evaluation of simplified propulsion-only emergency flight control system on transport aircraft. Technical report NASA/TM-1999-206578, NASA (1999) Google Scholar
  4. 65.
    De Gaay Fortman, W.F., Van Paassen, M.M., Mulder, M., In’t Veld, A.C., Clarke, J.P.: Implementing time-based spacing for decelerating approaches. J. Aircr. 44, 106–118 (2007) CrossRefGoogle Scholar
  5. 66.
    De Prins, J.L., Schippers, F.K.M., Mulder, M., Van Paassen, M.M., In’t Veld, A.C., Clarke, J.P.: Enhanced self-spacing algorithm for three-degree decelerating approaches. J. Guid. Control Dyn. 30, 576–90 (2007) CrossRefGoogle Scholar
  6. 80.
    Edwards, C., Lombaerts, T., Smaili, H.: Fault Tolerant Flight Control: A Benchmark Challenge vol. 399. Springer, Berlin (2010) CrossRefGoogle Scholar
  7. 91.
    Field, E.J., Pinney, T.R., (René) van Paassen, M.M., Stroosma, O., Rivers, R.A.: Effects of implementation variations on the results of piloted simulator handling qualities evaluations. In: AIAA Modeling and Simulation Technologies Conference and Exhibit, Providence, RI, USA, pp. 43–58 (2004) Google Scholar
  8. 105.
    Ganguli, S., Marcos, A., Balas, G.J.: Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis. In: American Control Conference, Anchorage, AK, USA, pp. 3612–3617 (2002) Google Scholar
  9. 113.
    Gouverneur, B., Mulder, J.A.B., van Paassen, M.M.R., Stroosma, O.: Optimization of the SIMONA Research Simulator’s Motion Filter Settings for Handling Qualities Experiments. In: AIAA Modeling and Simulation Technologies Conference and Exhibit, Austin, TX, USA (2003) Google Scholar
  10. 117.
    Hallouzi, R., Verhaegen, M.: Fault-tolerant subspace predictive control applied to a Boeing 747 model. J. Guid. Control Dyn. 31(4), 873–883 (2008) CrossRefGoogle Scholar
  11. 119.
    Hanke, C., Nordwall, D.: The simulation of a jumbo jet transport aircraft. Modelling data, vol. II. Technical report CR-114494/D6-30643-VOL2, NASA and The Boeing Company (1970) Google Scholar
  12. 125.
    Heerspink, H.M., Berkouwer, W.R., Stroosma, O., van Paassen, M.M., Mulder, M., Mulder, J.A.: Evaluation of vestibular thresholds for motion detection in the SIMONA research simulator. In: AIAA Modeling and Simulation Technologies Conference, San Francisco, CA, USA, pp. 1212–1231 (2005) Google Scholar
  13. 144.
    Joosten, D.A., van den Boom, T.J.J., Lombaerts, T.J.J.: Effective control allocation in fault-tolerant flight control using feedback linearization and model predictive control. In: European Control Conference (2007) Google Scholar
  14. 163.
    Lam, T.M., Mulder, M., Van Paassen, M.M., Mulder, J.A.: Comparison of control and display augmentation for perspective flight path displays. J. Guid. Control Dyn. 29, 564–578 (2006) CrossRefGoogle Scholar
  15. 172.
    Lombaerts, T.J.J., Chu, Q.P., Mulder, J.A., Joosten, D.A.: Real time damaged aircraft model identification for reconfiguring flight control. In: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Hilton Head, SC, USA, pp. 1207–1231 (2007) Google Scholar
  16. 173.
    Lombaerts, T.J.J., Huisman, H.O., Chu, Q.P., Mulder, J.A., Joosten, D.A.: Flight control reconfiguration based on online physical model identification and nonlinear dynamic inversion. In: AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, HI, USA (2008) Google Scholar
  17. 183.
    Marcos, A., Balas, G.J.: A Boeing 747-100/200 aircraft fault tolerant and diagnostic benchmark. Technical report AEM-UoM-2003-1, Department of Aerospace and Engineering Mechanics, University of Minnesota (2003) Google Scholar
  18. 194.
    Mulder, M., Veldhuijzen, A.R., Van Paassen, M.M., Mulder, J.A.: Integrating fly-by-wire controls with perspective flight path displays. J. Guid. Control Dyn. 28, 1263–1274 (2005) CrossRefGoogle Scholar
  19. 222.
    Shin, D., Moon, G., Kim, Y.: Design of reconfigurable flight control system using adaptive sliding mode control: actuator fault. Proc. Inst. Mech. Eng., G J. Aerosp. Eng. 219(4), 321–328 (2005), CrossRefGoogle Scholar
  20. 226.
    Shtessel, Y., Buffington, J., Banda, S.: Tailless aircraft flight control using multiple time scale re-configurable sliding modes. IEEE Trans. Control Syst. Technol. 10(2), 288–296 (2002) CrossRefGoogle Scholar
  21. 234.
    Smaili, M.H., Breeman, J., Lombaerts, T.J.J., Joosten, D.A.: A simulation benchmark for integrated fault tolerant flight control evaluation. In: AIAA Modeling and Simulation Technologies Conference and Exhibit, Keystone, CO, USA, pp. 563–585 (2006) Google Scholar
  22. 242.
    Stroosma, O., Smaili, H., Lombaerts, T., Mulder, J.A.: Piloted simulator evaluation of new fault-tolerant flight control algorithms for reconstructed accident scenarios. In: AIAA Modeling and Simulation Technologies Conference and Exhibit, Honolulu, HI, USA (2008) Google Scholar
  23. 243.
    Stroosma, O., van Paassen, M.M., Mulder, M.: Using the SIMONA research simulator for human-machine interaction research. In: AIAA Modeling and Simulation Technologies Conference, WA, USA (2003) Google Scholar
  24. 258.
    Valente Pais, A.R., Mulder, M., Van Paassen, M.M., Wentink, M., Groen, E.: Modeling human perceptual thresholds in self-motion perception. In: AIAA Modeling and Simulation Technologies Conference, Keystone, CO, USA, pp. 900–914 (2006) Google Scholar
  25. 261.
    Varga, A.: Design of least order residual generators for fault detection and isolation with application to monitoring actuator/surface faults for a Boeing 747 100/200 aircraft. Technical report DLR IB 515-08-28, DLR, 2008 Google Scholar
  26. 264.
    Vormer, F.J., Mulder, M., Van Paassen, M.M., Mulder, J.A.: Optimization of flexible approach trajectories using a genetic algorithm. J. Aircr. 43, 941–952 (2006) CrossRefGoogle Scholar
  27. 269.
    Wells, S.R., Hess, R.A.: Multi-input/multi-output sliding mode control for a tailless fighter aircraft. J. Guid. Control Dyn. 26(3), 463–473 (2003) CrossRefGoogle Scholar
  28. 288.
    Zaal, P.M.T., Nieuwenhuizen, F.M., Mulder, M., Van Paassen, M.M.: Perception of visual and motion cues during control of self-motion in optic flow environments. In: AIAA Modeling and Simulation Technologies Conference, Keystone, CO, USA, pp. 915–932 (2006) Google Scholar

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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