Publications



  1. Kier, T., Hofstee, J.: "VarLoads - Eine Simulationsumgebung zur Lastenberechnung eines voll flexiblen, freifliegenden Flugzeugs." Deutscher Luft- und Raumfahrtkongress, Dresden, September 2004, (2004) download
  2. Hecker, S.; Hahn, K. - U.: "Gust Computation System." AWIATOR, Technical Report, DLR-TR-3.1.1-11, Germany, May 2003
  3. Hahn, K. - U. ; Hecker, S.: "Gust Load Alleviation System."AWIATOR, Technical Report, DLR-TR-3.1.1-12, Germany, June 2003.
  4. Hofstee, J. Kier, T., Cerulli, C., Looye, G.: "A Variable, Fully Flexible Dynamic Response Tool for Special Investigations (VarLoads). " Proceedings International Forum on Aeroelasticity and Structural Dynamics 2003, Amsterdam, June 4-6, (2003).
  5. Looye, G., Joos, H.-D.: "Design of Autoland Controller Functions with Multi-Objective Optimization." Proc. of AIAA Guidance, Navigation, and Control Conference and Exhibit, August 5-8, 2002, Monterey, CA, (2002).
  6. Varga, A.: "Optimisation-based clearance." In C. Fielding, A. Varga, S. Bennani, M. Selier (Eds.), Advanced Techniques for Clearance of Flight Control Laws, Lect. Notes on Control and Information Sciences, vol. 283, pp. 107-117, Springer Verlag, 2002.
  7. Fielding, C., Varga, A., Bennani, S., Selier, M. (Eds.): "Advanced Techniques for Clearance of Flight Control Laws."Lect. Notes on Control and Information Sciences, vol. 283, Springer Verlag, 2002. Preface , Table of Contents.
  8. Moormann, D.: "The HIRM+ flight dynamics model." In C. Fielding, A. Varga, S. Bennani, M. Selier (Eds.), Advanced Techniques for Clearance of Flight Control Laws, Lect. Notes on Control and Information Sciences, vol. 283, pp. 121-139, Springer Verlag, 2002.
  9. Varga, A.: "Optimisation-based clearance: the linear analysis." In C. Fielding, A. Varga, S. Bennani, M. Selier (Eds.), Advanced Techniques for Clearance of Flight Control Laws, Lect. Notes on Control and Information Sciences, vol. 283, pp. 385-413, Springer Verlag, 2002.
  10. Joos, H.-D.; Looye, G.; and Willemsen, D.: "Application of an Optimization-based Design Process for Robust Autoland Control Laws Design." AIAA-Paper 2001-4206, Proc. AIAA Guidance, Navigation, and Control Conference, Montréal (Canada), 6-9 August 2001.
  11. Looye, G.; Joos, H.-D.; and Moormann, D.: "Automatic Tuning and Generation of Robust Dynamic Inversion Control Laws." AIAA-Paper 2001-4285, Proc. AIAA Guidance, Navigation, and Control Conference, Montréal (Canada), 6-9 August 2001.
  12. Looye, G.: "Design of Robust Autopilot Control Laws with Nonlinear Dynamic Inversion." at Automatisierungstechnik, 49, 12, (2001), pp.523-531
  13. Bauschat, J.-M. ; Mönnich, W.; Willemsen, D.; Looye, G.: "Flight Testing Robust Autoland Control Laws." AIAA-Paper 2001-4208, Proc. AIAA Guidance, Navigation, and Control Conference, Montréal (Canada), 6-9 August 2001.
  14. Bauschat, M.; and Joos, H.-D.: "Der sichere Autopilot - DLR-Landesystem schneller und wirtschaftlicher entwickelt." (in German) DLR-Nachrichten 99, November 2000.
  15. Joos, H.-D.; Looye, G.; Willemsen, D.; Mönnich, W., Bauschat; M.: "Automatisierte Auslegung eines robusten Autopilotensystems." DGLR Jahrestagung, Leipzig, September 2000.
  16. Joos, H.-D.: "A methodology for multi-objective design assessment and flight control synthesis tuning." Aerospace Science and Technology, 3, 3, (1999), pp.161-176.
  17. Joos, H.-D., Varga, A., Finsterwalder, R., Bals, J.: "Eine integrierte optimierungsbasierte Entwurfsumgebung für Flugregelungsaufgaben. " at - Automatisierungstechnik, 47. Jahrgang , 6, (1999), pp.239-248.
  18. Joos, H.-D., Finsterwalder, R.: "Multi-Objective Design Assessment and Control Law Synthesis Tuning for Flight Control." Development. Proc. IEEE International Symposium on Computer Aided Control System Design, Hawaii, August 22-27, pp.433-438, (1999).
  19. Looye, G.: "Integrated Flight Mechanics and Aeroelastic Aircraft Modeling using Object-Oriented Modeling Techniques." Proc. AIAA Modeling and Simulation Technology Conference, AIAA-99-4192, (1999).
  20. Moormann, D., Mosterman, P.J., Looye, G.: "Object-oriented computational model building of aircraft flight dynamics and systems." Aerospace Science and Technology, 3, 3, (1999), pp.115-126.
  21. Delgado Montes, I. et al.: "Robust Control Techniques, Tutorial Document. " GARTEUR/TP-088-07, 1997.
  22. Looye, G.; Bennani, S.; Moormann, D.; Varga, A.: "Post-Design Stability Robustness Assessment of the RCAM Controller Design Entries." GARTEUR/TP-088-35, 1997.
  23. Varga, A.; Moorman, D.; Grübel, G.; Looye, G.: "Automated Generation of LFT-based Parametric Uncertainty Descriptions from Generic Aircraft Models." GARTEUR/TP-088-36, 1997.
  24. Kienitz, K.H.: "HIRM Design Challenge Presentation Document: A Combined Multimodel-Multicriteria-LQG/LTR Approach."
  25. Kienitz, K.H.; Grübel, G.: "Mehrzielige Regleroptimierung für das 'High Incidence Research Model' der GARTEUR 'Design Challenge on Robust Flight Control'". Proc. Deutscher Luft- und Raumfahrtkongress 1997, München. Contributions to the book: "Robust Flight Control - A design challenge", Springer, Lecture Notes in Control and Information Science 224, 1997:
  26. Grübel, G.; and Joos, H.-D.: "Multi-Objective Parameter Synthesis (MOPS)".
  27. Lambrechts, P.; Bennani, S.; Looye, G. and Moormann, D.: "The RCAM Design Challenge Problem Description."
  28. Grübel, G.: "Another View on the Design Challenge Achievements."
  29. Helmersson, A. et al.: "Robust Flight Control Design Challenge, Problem Formulation and Manual: the Research Civil Aircraft Model (RCAM)." GARTEUR/TP-088-03, 1996.
  30. Irving, J.P. et al.: "Robust Flight Control Design Challenge, Problem Formulation and Manual: the High Incidence Research Model (HIRM)." GARTEUR/TP-088-04, 1996.
  31. Joos, H.D.: "RCAM Design Challenge Presentation Document: Multi-Objective Parameter Synthesis (MOPS)." GARTEUR/TP-088-16, 1996.


URL for this article
http://www.dlr.de/rm/en/desktopdefault.aspx/tabid-3796/5976_read-8772/