Try Mobilus Beta
Search tips
 This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Cessna Citation X Engine Model Identification from Flight Tests

Journal Article
2015-01-2390
ISSN: 1946-3855, e-ISSN: 1946-3901
DOI: https://doi.org/10.4271/2015-01-2390
Published September 15, 2015 by SAE International in United States
Cessna Citation X Engine Model Identification from Flight Tests
Sector:
Citation: Ghazi, G., Botez, R., and Messi Achigui, J., "Cessna Citation X Engine Model Identification from Flight Tests," SAE Int. J. Aerosp. 8(2):203-213, 2015, https://doi.org/10.4271/2015-01-2390.
Language: English

References

  1. Daniel , P.R. Aircraft design: a conceptual approach Published by American Institute of Aeronautics and Astronautics Inc 515 552 1992
  2. Hill , P.G. and Peterson , C.R. Mechanics and thermodynamics of propulsion Reading, MA Addison-Wesley Publishing Co. 1992 1 1992
  3. Ghazi , G. Développement d'une plateforme de simulation et d'un pilote automatique - application aux Cessna Citation X et Hawker 800XP Master thesis University of Quebec - École Polytechnique de Montréal Montreal, Quebec 2014
  4. Rodriguez , L.F. and Botez , R.M. Civil turbofan engines thrust generic model IECON 2012-38th Annual Conference on IEEE Industrial Electronics Society 2012 5444 5450
  5. Murrieta-Mendoza , A. , Botez , R. , Labour , D. Vertical Navigation Trajectory Optimization Algorithm for the Lockheed L-1011 the AIAA Aicraft Noise and Emissions Reduction Symposium Atlanta, GA 2014
  6. Murrieta-Mendoza , A. and Botez , R. Navigation Trajectory Optimization Algorithm For A Commercial Aircraft the AIAA/3AF Aircraft Noise and Emissions Reduction Symposium 2014
  7. Murrieta-Mendoza , A. and Botez , R. Method to Calculate Aircraft VNAV Trajectory cost Using a Performance Database International Mechanical Engineering Congress & Exposition Montreal, Canada 2014
  8. Murrieta-Mendoza , A. , Demange , S. , George , F. , and Botez , R. Performance DataBase creation using a level D simulator for Cessna Citation X aircraft in cruise regime IASTED Modeling, Identification and Control Conference Innsbruck, Austria 2015
  9. Wanner , J.-C. Dynamique du vol et pilotage des avions Office national d'études et de recherches aérospatiales ONERA 1 205 0078-379X 1983
  10. Mattingly , J.D. , Heiser , W.H. , Daley , D. H. Aircraft Engine Design AIAA Education series 1987
  11. Yadav , R. , Kapadi , Y. , Pashilkar , A. Aero-thermodynamic model for digital simulation of turbofan engine ASME Turbo Expo 2005: Power for Land, Sea, and Air 2005 63 70
  12. Roberts , R.A. and Eastbourn , S.M. Modeling Techniques for a Computational Efficient Dynamic Turbofan Engine Model International Journal of Aerospace Engineering 2014 11 2014
  13. May , R.D. , Csank , J. , Lavelle , T. M. A high-fidelity simulation of a generic commercial aircraft engine and controller rs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20100037767.pdf 2010
  14. Cook , M.V. Flight dynamics principles: a linear systems approach to aircraft stability and control Butterworth-Heinemann 2012
  15. Nelson , R.C. Flight stability and automatic control 2 WCB/McGraw Hill 1998
  16. Félix Patrón , R.S. , Botez , R.M. , Labour , D. New altitude optimisation algorithm for the flight management system CMA-9000 improvement on the A310 and L-1011 aircraft Aeronautical Journal 117 787 805 2013
  17. Félix Patrón , R.S. , Botez , R.M. , Labour , D. Vertical profile optimization for the Flight Management System CMA-9000 using the golden section search method IECON 2012-38th Annual Conference on IEEE Industrial Electronics Society Proceedings 2012 5482 5488
  18. Félix Patrón , R.S. , Kessaci , A. , Botez , R. M. , Labour , D. Flight trajectories optimization under the influence of winds using genetic algorithms AIAA Guidance, Navigation, and Control (GNC) Conference Proceedings 2013
  19. Félix Patrón , R.S. , Oyono Owono , A. C. , Botez , R. M. , Labour , D. Speed and altitude optimization on the FMS CMA-9000 for the Sukhoi Superjet 100 using genetic algorithms Aviation Technology, Integration, and Operations Conference Proceedings 2013
  20. Dancila , B. , Botez , R. , Labour , D. Fuel burn prediction algorithm for cruise, constant speed and level flight segments Aeronautical Journal 117 491 504 2013
  21. Dancila , B. , Botez , R. , Labour , D. Altitude optimization algorithm for cruise, constant speed and level flight segments École de technologie supérieure 2011
  22. Dancila , R. , Botez , R. , Ford , S. Fuel burn and emissions evaluation for a missed approach procedure performed by a B737-400 Aviation Technology, Integration, and Operations (ATIO) Conference and International Powered Lift Conference (IPLC) 2013 12 14
  23. Hamel , C. , Botez , R. , and Ruby , M. Cessna Citation X Airplane Grey-Box Model Identification without Preliminary Data SAE Technical Paper 2014-01-2153 2014 10.4271/2014-01-2153
  24. Hamel , C. , Botez , R. , Ruby , M. Cessna Citation X Grey-Box New Aerodynamic Model Identification from Flight Test
  25. Hamel , C. , Sassi , A. , Botez , R. , and Dartigues , C. Cessna Citation X Aircraft Global Model Identification from Flight Tests SAE Int. J. Aerosp. 6 1 106 114 2013 10.4271/2013-01-2094
  26. Rodriguez , L.F. and Botez , R.M. Generic New Modeling Technique for Turbofan Engine Thrust Journal of Propulsion and Power 29 1492 1495 2013
  27. Gong , C. and Chan , W.N. Using flight manual data to derive aero-propulsive models for predicting aircraft trajectories Proc. of AIAA's Aircraft Technology, Integration, and Operations (ATIO) Forum Los Angeles, CA 2002
  28. Mota , S.D.J. and Botez , R.M. New identification method based on neural network for helicopters from flight test data AIAA Atmospheric Flight Mechanics Conference Chicago, Illinois 2009 10 13
  29. Mota , S.D.J. and Botez , R.M. New helicopter model identification method based on flight test data Aeronautical Journal 115 295 2011
  30. Mota , S.D.J. , Nadeau Beaulieu , M. , Botez , R. M. Identification of a MIMO state space model of an F/A-18 aircraft using a subspace method Aeronautical Journal 113 183 2009
  31. Boëly , N. and Botez , R. M. New approach for the identification and validation of a nonlinear F/A-18 model by use of neural networks IEEE Transactions on Neural Networks 21 1759 1765 2010
  32. Boely , N. , Botez , R.M. , Kouba , G. Identification of a non-linear F/A-18 model by the use of fuzzy logic and neural network methods Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 225 559 574 2011
  33. Boughari , Y. , Botez , R. , Ghazi , G. , and Theel , F. Evolutionary Algorithms for Robust Cessna Citation X Flight Control SAE Technical Paper 2014-01-2166 2014 10.4271/2014-01-2166
  34. Boughari , Y. , Botez , R. , Theel , F. , Ghazi , G. Optimal flight control on Cessna Citation X aircraft using differential evolution 33nd IASTED International Conference on Modeling, Identification and Control (MIC) Innsbruck, Austria
  35. Ghazi , G. and Botez , R. New robust control analysis methodology for Lynx helicopter and Cessna Citation X aircraft using Guardian Maps, Genetic Algorithms and LQR theories combinations American Helicopter Society AHS 70th Annual Forum Montréal, Quebec 2014
  36. Ghazi , G. and Botez , R.M. Lateral Controller Design for the Cessna Citation X with Handling Qualities and Robustness Requirements 62nd Canadian Aeronautical Society Institute CASI Aeronautics Conference and AGM Montreal, Quebec, Canada 2015
  37. Klein , V. and Morelli , E. A. Aircraft system identification: theory and practice American Institute of Aeronautics and Astronautics Reston VA, USA 2006
  38. Jategaonkar , R.V. and Thielecke , F. Aircraft parameter estimation-A tool for development of aerodynamic databases Sadhana 25 119 135 2000
  39. Zadeh , L.A. From circuit theory to system theory Proceedings of the IRE 50 856 865 1962
  40. Roux , E. Pour une approche analytique de la dynamique du vol Ph.D. Thesis, SUPAERO-ONERA, École Nationale Supérieure de l'Aéronautique et de l'Espace 2005
  41. Stevens , B. L. and Lewis , F. L. Aircraft control and simulation John Wiley & Sons 2003
  42. Brumbaugh , R. W. Aircraft model for the AIAA controls design challenge Journal of guidance, control, and dynamics 17 747 752 1994
  43. Jategaonkar , R. V. Flight Vehicle System Identification a Time Domain Methdology Reston, VA American Institute of Aeronautics and Astronautics 2006
  44. Klein , V. Estimation of aircraft aerodynamic parameters from flight data Progress in Aerospace Sciences 26 1 77 1989
  45. Clerc , M. Particle swarm optimization 93 John Wiley & Sons 2010
  46. Poli , R. , Kennedy , J. , Blackwell , T. Particle swarm optimization Swarm intelligence 1 33 57 2007
  47. Oates , G. C. Aerothermodynamics of gas turbine and rocket propulsion AIAA Educations Series 1997

Cited By