Publications

Pour plus des détails à jour sur les articles publiés, svp visitez le site web de Research Gate à: http://www.researchgate.net/profile/Ruxandra_Botez
 

 
Articles soumis dans des revues avec comité de lecture
 
  1. Boughari, Y., Ghazi, G., Botez, R. M., Theel, F., 2016, New Methodology for Optimal Flight Control using Differential Evolution - Application to the Cessna X Aircraft, ” Aeronautical Journal  


 

Articles acceptés, sous presse et publiés dans des revues avec comité de lecture
 
  1. Mosbah, A. B., Botez, R. M., Dao, T. M., 2016, New Methodology combining Neural Network and Extended Great Deluge Algorithms for the ATR-42 Wing Aerodynamics Analysis, ” The Aeronautical Journal, Vol. 120(1229), pp. 1049-1080.  

  2. Murrieta-Mendoza, A., Botez, R. M., Ford, S., 2016, New method to compute the missed approach fuel consumption and its emissions, ” The Aeronautical Journal,Vol. 120(1228), pp. 910 - 929.  

  3. Koreanschi, A., Sugar-Gabor, O., Botez, R. M., 2016, Numerical and Experimental Validation of a Morphed Wing Geometry Using Price-Païdoussis Wind Tunnel Testing, ” The Aeronautical Journal, Vol. 120(1227), pp. 757- 795.  

  4. Boughari, Y., Botez, R. M., Ghazi, G., Theel, F., 2016, Flight Control Clearance of the Cessna Citation X using Evolutionary Algorithms, ” Proceedings of the Institute of Mechanical Engineers IMechE, Part G: Journal of Aerospace. Proceedings of the Institute of Mechanical Engineers IMechE, Part G: Journal of Aerospace, Published online before print April 11, 2016, doi: 10.1177/0954410016640821.  

  5. Dancila, B. D., Botez, R. M., 2016, “Geographic Area Selection and Construction of a corresponding Routing Grid used for in-Flight Management System Flight Trajectory Optimization, ” Proceedings of the Institute of Mechanical Engineers IMechE, Part G: Journal of Aerospace. Published online before print, April 13, 2016, doi:10.1177/0954410016643104 

  6. Sugar Gabor, O., Koreanschi, A., Botez, R. M., Mamou, M., Mébarki, Y., 2016, Numerical Simulation and Wind Tunnel Tests Investigation and Validation of a Morphing Wing-Tip Demonstrator Aerodynamic Performance, ” Aerospace Science and Technology, Vol. 53, June 2016, Pages 136–153.  

  7. Koreanschi, A., Sugar-Gabor, O., Botez, R. M., 2016, Drag Optimization of a Wing Equipped with a Morphing Upper Surface, ” The Aeronautical Journal, Vol. 120(1225), pp. 473-493.  

  8. Murrieta-Mendoza, A., Gagné, J., Botez, R. M., 2016, New Search Space Reduction Algorithm for Vertical Reference Trajectory Optimization, ” INCAS Bulletin, Vol. 8(2), pp. 77-95.  

  9. Mosbah, A. B., Botez, R. M., Dao, M. T., Guezguez, M., Zaag, M., 2016, A Neural Network Controller New Methodology for the ATR-42 Morphing Wing Actuation, ” INCAS Bulletin, Vol. 8(2), pp. 59-75.  

  10. Koreanschi, A., Henia, M. B., Guillemette, O., Michaud, F., Tondji, Y., Sugar Gabor, O., Botez, R. M., Flores Salinas, M., 2016, Flutter Analysis of a Morphing Wing Technology Demonstrator: Numerical Simulation and Wind Tunnel Testing, ” INCAS Bulletin, Vol. 8(1), pp. 99-124.  

  11. Sugar Gabor, O., Simon, A., Koreanschi, A., Botez, R. M., 2016, Aerodynamic Performance Improvement of the UAS-S4 Éhecatl Morphing Airfoil using Novel Optimization Techniques, ” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 230(7), pp. 1164-1180.  

  12. Sugar Gabor, O., Simon, A., Koreanschi, A., Botez, R. M., 2016, Improving the UAS-S4 Éhecatl airfoil high angle of attack performance characteristics using a morphing wing approach, ” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 23(2), pp. 118-131.  

  13. Mosbah, A. B., Botez, R. M., Dao, T. M., 2016, Hybrid Original Approach for the Prediction of the Aerodynamic Coefficients of an ATR-42 Scaled Wing Model,” Chinese Aeronautical Journal, Vol. 29(1), pp. 41-52.  

  14. Ghazi, G., Botez, R., Achigui, J. M., 2015, Cessna Citation X Engine Model Identification from Flight Tests,” SAE International Journal of Aerospace, Vol. 8 (2015-01-2390).  

  15. Tchatchueng Kammegne, M. J., Grigorie, L. T., Botez, R. M., 2015, Design, Numerical Simulation and Experimental Testing of a Controlled Electrical Actuation System in a Real Aircraft Morphing Wing Model,” The Aeronautical Journal, Vol. 119(1219).  

  16. Koreanschi, A., Sugar-Gabor, O., Botez, R. M., 2015, Drag Optimization of a Wing Equipped with a Morphing Upper Surface,” The Aeronautical Journal.  

  17. Felix Patron, R. S., Botez, R. M., 2015, Flight Trajectories Optimization through Genetic Algorithms New Methodology for Vertical and Lateral Profiles Coupling, AIAA Journal of Aerospace Information Systems.  

  18. Murrieta Mendoza, A., Botez, R. M., 2015, New Methodology for an Aircraft Vertical Navigation Flight Trajectory Cost calculation using a Performance Database, AIAA Journal of Aerospace Information Systems.  

  19. Edu, I. R., Adochiei, F. C., Grigorie, T. L., Botez, R. M., 2015, Tuning of a Wavelet Filter for Miniature Accelerometers Denoising based Joint Symbolic Dynamics (JSD) Method, INCAS Bulletin, Vol. 7(2), pp. 71-80, ISSN 2066-8201.  

  20. Anton, N., Botez, R. M., 2015, Weight Functions Method for Stability Analysis applied as Design Tool for Hawker 800XP Aircraft, The Aeronautical Journal, Vol. 119(1218), pp. 981-999.  

  21. Grigorie, T. L., Botez, R. M., 2015,Positioning Monitoring Improvement in a Horizontal Plane INS by Using Fuzzy Logic Data Fusion for Denoising of Inertial Sensors in Redundant Clusters, International Journal of Fuzzy Systems and Advanced Applications, Vol. 2, pp. 33-40, ISSN 2313-0512.  

  22. Tchatchueng Kammegne, M. J., Grigorie, L. T., Botez, R. M., Koreanschi, A., 2015, Design and Wind Tunnel Experimental Validation of a Controlled New Rotary Actuation System for a Morphing Wing Application, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, published on 1st of June.  

  23. Sugar Gabor, O., Simon, A., Koreanschi, A., Botez, R. M., 2015, Improving the UAS-S4 Éhecatl airfoil high angles of attack performance characteristics using a morphing wing approach, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, published, 2nd of June.  

  24. Grigorie, L.T., Botez, R.M., Popov, A.-V., 2015,How the Airfoil Shape of a Morphing Wing is Actuated and Controlled in a Smart Way, The Journal of Aircraft Engineering, ASCE Edition, Vol. 28(1).  

  25. Ren, Q., Baron, L., Balazinski, M., Botez, R., Bigras, P., 2015,Tool wear assessment based on type-2 fuzzy uncertainty estimation on acoustic emission, Applied Soft Computing, Vol. 31, pp. 14-24.  

  26. Felix Patron, R. S., Berrou, Y., Botez, R. M., 2015, New Methods of Optimization of the Flight Profiles for Performance Database-Modeled Aircraft, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 229, pp. 1853-1867, first published on December 2, 2014 doi:10.1177/0954410014561772.  

  27. Dancila, R., Botez, R. M., Ford, S., 2014, Fuel burn and emissions evaluation for a missed approach procedure performed by a B737-400, The Aeronautical Journal,Vol. 118(1209).  

  28. Patron, R F., Kessaci, A,, Botez, R. M., 2014, Horizontal flight trajectories optimization for the aircraft A-310, L-1011 and SSJ100, The Aeronautical Journal, Vol. 118(1210. 

  29. Ren, Q., Balazinski, M., Baron, L., Jemielniak, K., Achiche, A., Botez, R., 2013, Type 2 Fuzzy Tool Condition Monitoring System Based on Acoustic Emission in Micromilling, Information Sciences, Vol. 255, pp. 121-134.  

  30. Fays, J., Botez, R.M., 2013, Algorithm for the aircraft trajectories considering No-Fly-Zones for a Flight Management System, The INCAS Bulletin, Vol. 5(3), 

  31. Sugar Gabor, O., Koreanschi, A., Botez, R, T., 2013, Optimization of an Unmanned Aerial System' Wing Using a Flexible Skin Morphing Wing, SAE International Journal of Aerospace, Vol. 6(1), pp. 115-121, 

  32. Mosbah, A., B., Flores Salinas, M., Botez, R., Dao, T., 2013, ,New Methodology for Wind Tunnel Calibration Using Neural Networks - EGD Approach, SAE International Journal of Aerospace, Vol. 6(2), 

  33. Rodriguez Fajardo, L., Botez, R. M., 2013, Generic new modelling technique for turbofan engines thrust, The Journal of Aircraft Engineering ASCE, The AIAA Journal of Propulsion and Power, Vol. 29(6). pp. 1492-1495. 

  34. Hamel, C., Sassi, A., Botez, R., Dartigues, C., 2013, Cessna Citation X aircraft global model identification from fight tests, SAE International Journal of Aerospace 6(1):106-114, 2013, doi:10.4271/2013-01-2094.

  35. Grigorie, L.T., Botez, R.M., Popov, A.-V., 2013, How the airfoil shape of a morphing wing is actuated and controlled in a smart way, Journal of Aircraft Engineering, ASCE, 10.1061/(ASCE)AS.1943-5525.0000372. ASENG-589.

  36. Dancila, B., Botez, R.M., Labour, D., 2013, Fuel burn prediction algorithm for cruise, constant speed and level flight segments, The Aeronautical Journal, Vol. 117, No 1191, pp. 491-503.

  37. Anton, N., Botez, R. M., Popescu, D., 2013, Application of the weight function method on a high incidence research aircraft model, The Aeronautical Journal, Vol. 117, No 1195, pp. 897-912.

  38. Patron Felix, S. R., Botez, R. M., 2013, New altitude optimization algorithm for the Flight Management System CMA-9000 improvement on the A310 and L-1011 aircraft, The Aeronautical Journal Vol. 177, No 1194, pp. 787-805.

  39. Grigorie, L. T., Botez, R. M., 2013, A new method to reduce the noise of the miniaturized inertial sensors disposed in redundant linear configurations, The Aeronautical Journal, Vol. 117, No 1188, pp. 111-132.

  40. Botez, R.M., Hiliuta, A., Stathopoulos, N., Thérien, S., Rathé, A., Dickinson, M., 2012, Aeroservoelastic flutter and frequency response interactions on the CL-604 aircraft, INCAS Bulletin, Vol. 4, Issue 4. pp. 15-122.

  41. Grigorie, L. T., Botez, R. M., Popov, A.-V., Mamou, M., Mébarki, Y., 2012, A hybrid fuzzy logic proportional-integral-derivative and conventional on-off controller for morphing wing actuation using shape memory alloy, Part 1: Morphing system mechanisms and controller architecture design, The Aeronautical Journal, Vol. 116 (1179), pp. 433-449.

  42. Grigorie, L. T., Botez, R. M., Popov, A.-V., Mamou, M., Mébarki, Y., 2012, A hybrid fuzzy logic proportional-integral-derivative and conventional on-off controller for morphing wing actuation using shape memory alloy, Part 2: Controller implementation and validation, The Aeronautical Journal, Vol. 116 (1179), pp. 451-465.

  43. Grigorie, L. T., Botez, R. M., 2012, A new method to reduce the noise of the miniaturized inertial sensors disposed in redundant linear configurations, The Aeronautical Journal.

  44. Courchesne, S., Popov, A.-V., Botez, R. M,. 2012, New aeroelastic studies for a morphing wing, INCAS Bulletin, Vol. 4(2), 19-28.

  45. Grigorie, L. T., Botez, R. M., Lungu, M., Edu, R. I., Obreja, R., 2012, MEMS gyro performance improvement through bias correction over temperature using an adaptive neural network trained fuzzy inference system, Proceedings of the Institution of Mechanical Engineers, Part G, Journal of Aerospace Engineering, pp. 1-18.

  46. Grigorie, L.T., Popov, A.-V., Botez, R. M., Mamou, M., Mebarki, Y., 2012, On-Off and Proportional-Integral Controller for a Morphing Wing. Part 1: actuation mechanism and control design, Proceedings of the Institution of Mechanical Engineers, Vol. 226(2), Part G, Journal of Aerospace Engineering, pp. 131-145.

  47. Grigorie, L.T., Popov, A.-V., Botez, R. M., Mamou, M., Mebarki, Y., 2012, On-Off and Proportional-Integral Controller for a Morphing Wing. Part 2: control validation - numerical simulations and experimental tests, Proceedings of the Institution of Mechanical Engineers, Vol. 226(2), Part G, Journal of Aerospace Engineering, pp. 146-162.

  48. Anton, N., Botez, R. M., 2011, Weight Functions Method Application on a Delta-Wing X-31 configurations, INCAS Bulletin, Vol. 3(4), pp. 3-16, ISSN 2066-8201.

  49. De Jesus Mota, S., Botez, R.M., 2011, New helicopter model identification method based on a neural network optimization algorithm and on flight test data, The Aeronautical Journal, Vol. 115, No. 1167, pp. 295-314.

  50. Anton, N., Botez, R. M., Popescu, D., 2011, Stability derivatives for X-31 delta-wing aircraft validated using wind tunnel test data, Proceedings of the Institution of Mechanical Engineers,Vol. 225, Part G, Journal of Aerospace Engineering, pp 403-416.

  51. Boely, N., Botez, R.M., Kouba, G., 2011, Identification of a nonlinear F/A-18 model by use of fuzzy logic and neural network methods, Proceedings of the Institution of Mechanical Engineers, Vol. 225, Part G, Journal of Aerospace Engineering, pp. 559-574.

  52. Popov, A.V., Botez, R.M., Grigorie, T. L., Mamou, M., Mebarki, Y., 2010, Modeling and testing of a morphing wing in an open loop architecture, AIAA Journal of Aircraft, Vol. 47(3), pp. 917-923.

  53. Boely, N., Botez, R.M., 2010, New approach for the identification and validation of a nonlinear F/A-18 model by use of neural networks, IEEE Transactions on Neural Networks, Vol. 21(11), pp.1759-1765.

  54. Anton, N., Popescu, D., Botez, R.M., 2010 New methods and code for stability derivatives calculations from Hawker 800 XP aircraft geometrical data knowledge,The Aeronautical Journal, Vol. 114(1156).

  55. Silisteanu, P, Botez, R.M., 2010, New methodology for transition studies, AIAA Journal of Aircraft, Vol. 47(2), pp. 703-707.

  56. Popov, A.V., Botez, R.M., Grigorie, T. L., Mamou, M., Mebarki, Y., 2010, Real time airfoil optimization of a morphing wing in wind tunnel, AIAA Journal of Aircraft, Vol. 47(4), pp. 1346-1354.

  57. Popov, A.-V., Botez, R. M., Grigorie, T. L., Mamou, M., Mebarki, Y., 2010, Closed loop control of a morphing wing in wind tunnel, AIAA Journal of Aircraft , Vol. 47(4), pp. 1309-1317.

  58. Grigorie, L.T., Botez, R.M., 2010, Modelling and numerical simulation of an algorithm for the inertial sensors errors reduction and for the increase of the strap-down navigator redundancy degree in a low cost architecture, sous presse, CSME Transactions, Vo . 34(1), pp. 1-16.

  59. Grigorie, L.T., Botez, R.M., 2010, New adaptive controller method for SMA hysteresis modeling of a morphing wing, The Aeronautical Journal, Vol. 114(1151), pp. 1-13,.

  60. Kouba, G., Botez, R.M., Boely, N., 2009, Fuzzy logic method use in the F/A-18 aircraft model identification, sous presse, AIAA Journal of Aircraft, Vol. 47(1), pp. 1-17.

  61. Grigorie, L.T., Botez, R.M., Popov, A.-V., 2009, Adaptive neuro-fuzzy controllers for an open loop morphing wing system. Journal of Aerospace Engineering, Vol. 223(J), pp. 965-975.

  62. Grigorie, L.T., Botez, R.M., 2009, Adaptive neuro-fuzzy inference system based controllers for Smart Material Actuator modeling, Journal of Aerospace Engineering, Vol. 223(G6), pp. 655-668

  63. Popov, A-V., Botez, R. M., Mamou, M., Grigorie, L.T., 2009, Optical sensor pressure measurements variations with temperature in wind tunnel testing, AIAA Journal of Aircraft, Vol. 46(4), pp.1314-1318.

  64. De Jesus Mota, S., Beaulieu-Nadeau, M., Botez, R.M., 2008, Identification of a MIMO state space model of an F/A-18 aircraft using a subspace method, Royal Aeronautical Journal, Vol. 112(1142) .

  65. Grigorie, L. T., Botez, R. M., 2008, The bias temperature dependence estimation and compensation for an accelerometer by use of the neuro-fuzzy techniques, Canadian Society for Mechanical Engineering Transactions, Vol. 32(3), pp. 383-400.

  66. Botez, R.M., Hiliuta, A., Grigorie, L., Ciocan, L., 2008, Validation of a simulation method for rigid and control aerodynamic unsteady forces for aeroservoelasticity interactions studies, AIAA Journal of Guidance, Control, and Dynamics, Vol. 31(5), pp. 1372-1385.

  67. Popov. A-V., Labib, M., Fays, J., Botez, R.M., 2008, Closed loop control simulations on a morphing laminar airfoil using shape memory alloys actuators, AIAA Journal of Aircraft, Vol. 45(5), pp. 1794-1803.

  68. Nadeau Beaulieu, M., Botez, R.M., 2008, Simulation and prediction of the helicopter main rotor, tail rotor and engine parameters by using the subspace system identification method, Journal of Aerospace Engineering, Vol. 222(G6), pp. 817-834.

  69. Popov, A. V., Botez, R.M., Labib, M., 2008, Transition point detection from the surface pressures distribution for controller design, AIAA Journal of Aircraft, Vol. 45(1), pp. 23-28.

  70. Biskri, D.E., Botez, R.M., 2007, Method for aerodynamic unsteady forces time calculations on an F/A-18 aircraft, The Aeronautical Journal, Vol. 112 (1127), pp. 1-6.

  71. Nadeau Beaulieu M., Botez, R. M., Hiliuta, A., 2007, Ground dynamics model validation by use of landing flight test, AIAA Journal of Aircraft, Vol. 44(6), pp. 2063-2068.

  72. Biskri, D.E., Botez, R.M., Thérien, S., Rathé, A., Stathopoulos, N., Dickinson, M., 2007, Aeroservoelasticity analysis method based on an error analytical form, Journal of Vibration and Control, Vol. 14(8), pp. 1217-1230..

  73. Nadeau Beaulieu, M., De Jesus Mota, S., Botez, R.M., 2006, Identification of structural surfaces positions on an F/A-18 using the subspace identification method from flight flutter tests, Journal of Aerospace Engineering, Special Issue, Vol. 221, pp. 719-731.

  74. Hiliuta, A., Botez, R. M., 2007, Flight dynamics helicopter model validation based on flight test data,Journal of Aerospace Engineering, Vol. 221(5), pp. 757-765.

  75. Botez, R.M., Dinu, A., Cotoi, I., 2007, Method based on Chebyshev polynomials for aerservoelastic Interactions on an F/A-18 Aircraft, AIAA  Journal of Aircraft, Vol. 44(1), pp. 330-333.

  76. Botez, R. M., Biskri, D.E., 2007, Unsteady aerodynamic forces mixed method for aeroservoelasticity studies on an F/A-18 aircraft, AIAA Journal of Aircraft, Vol. 44(4), pp. 1378-1383.

  77. Botez, R. M., Dinu, A., Cotoi, I., Stathopoulos, N., Terrien, S., Rathé, A., Dickinson, M., 2007,  Improved method for creating time-domain unsteady aerodynamic models, The Journal of Aerospace Engineering Vol. 20(3), pp. 204-206.

  78. Botez, R. M., Rotaru, M., 2007, Relationships between Flying qualities and Flight test parameters for the F/A-18 aircraft, The Aeronautical Journal, Vol. 111 (1118), pp. 231-232.

  79. Grigorie, T. L., Hiliuta, A., Botez, R.M., Aron, I.,2006, Numerical and experimental study of an algorithm of attitude for a strap down inertial system, Canadian Society for Mechanical Engineering Journal, Vol. 30, No. 3, pp. 429-442.

  80. Biskri, D.E., Botez, R.M., 2006, Aerodynamic forces based on an error analytical formulation for aeroservoelasticity studies on an F/A-18 aircraft, Journal of Aerospace Engineering, Vol. 220 (G), pp. 421-428.

  81. Biskri, D.E., Botez, R.M., Stathopoulos, N., Thérien, S., Rathé, A., Dickinson, M., 2006, New mixed method for unsteady aerodynamic force approximations for aeroservoelasticity studies, AIAA Journal of Aircraft, Vol. 43(5), pp. 1538-1542.

  82. Dinu, A., Botez, R. M., Cotoi, I., 2006, Chebyshev Polynomials for unsteady aerodynamic calculations in aeroservoelasticity, AIAA Journal of Aircraft, Vol. 43(1), pp. 165-171.

  83. Dinu, A., Botez, R.M., Cotoi, I., 2005, Aerodynamic forces approximations by Chebyshev method for aeroservoelasticity studies, Canadian Aeronautical Society Journal CASJ, Vol. 51(4), pp. 167-175.

  84. Hiliuta, A., Botez, R.M., Brenner, M., 2005, Approximation of unsteady aerodynamic forces Q(k, M) by use of fuzzy techniques, AIAA Journal,  Vol. 43(10), pp. 2093-2099.

  85. Ibrir, S., Botez, R. M., 2005, Robust stabilization of uncertain aircraft systems with linear model, Journal of Vibration and Control, Vol. 11, pp.187-200.

  86. Dumitrache, A., Botez, R. M., 2005, Active control laws for aeroelasticity, PAMM, Vol. 5(1), pp. 651-652.

  87. Botez, R. M., Biskri, Doin, A., D.E., Cotoi, I., Parvu, P., 2004, Closed loop aeroservoelastic analysis method, AIAA Journal of Aircraft, Vol. 41(4), pp. 962-964.

  88. Botez, R., M., Doin, A., Biskri, D., Cotoi, I., Hamza, D., Parvu, P., 2003, Method for flutter aeroservoelastic open loop analysis, Canadian Aeronautical Society Journal CASJ, Vol. 49(4),  pp. 179-190.

  89. Cotoi, I., Botez, R. M., 2002, Method of unsteady aerodynamic forces approximation for aeroseroelastic interactions, AIAA Journal of Guidance, Control, and Dynamics Scope, Vol. 25(5), pp. 985-987.

  90. Aouf, N., Boulet, B., Botez, R., 2002, Model and controller reduction for  flexible  aircraft preserving robust performance, IEEE Transactions on Control Systems Technology, Vol. 10(2), pp. 229-237.

  91. Botez, R. M., Chelaru, V., Pârvu, P., Gheorghe, C., 2001, Calculus model for a  rolling guided missile, Journal of Vibration and Control, Vol. 7, pp. 863-889.

  92. Botez, R. M., Boustani, I., Vayani, N., Bigras, P., Wong, T., 2001, Optimal control laws for gust alleviation, Canadian Aeronautical Society Journal, Vol. 47 (1), pp. 1-6.

  93. Aouf, N., Boulet, B., Botez, R., 2000, Robust gust load alleviation for a flexible aircraft, Canadian Aeronautical Society Journal, Vol. 46 (3), pp. 131-139 (article en page couverture de nr.).

  94. Wong, T., Houle, J.-L., Botez, R.M., 2000, Complexity of a class of task scheduling  problems, Libertas Matematica, Vol. XX, pp. 131-139.

  95. Botez, R.M., Bigras, P., 1999, Methods for the aerodynamic approximation in the Laplace domain for the aeroservoelastic studies, Libertas Matematica, Vol. XIX,   pp. 171-181.

  96. Botez, R.M. et Païdoussis, M.P., 1996, Dynamics of an articulated cylinder in annular flow via non-linear and partially linearized versions of an analytical model,Journal of Sound and Vibration, Vol. 192 (3), pp. 645-668.

  97. Païdoussis, M.P., Botez, R.M., 1995, Three routes to chaos for a three-degree-of-freedom articulated cylinder system subjected to annular flow and impacting on the outer pipe, Journal of Nonlinear Dynamics, Vol. 7, pp. 429-450.

  98. Païdoussis, M.P., Botez, R.M., 1993, Chaotic dynamics of articulated cylinders in confined axial flow, Journal of Fluids and Structures, Vol. 7, pp. 719-750.




 
Articles acceptés et publiés dans des comptes rendus de conférence avec arbitrage

  1. Nguyen, D. H., Tchatchueng Kammegne, M. J., Botez, R. M., Grigorie, L., 2016,Open Loop Morphing Wing Architecture based ANFIS Controller, 16th AIAA Aviation Technology, Integration, and Operations Conference, Washington, DC, Etats-unis, 13-17 juin.

  2. Tchatchueng Kammegne, M. J., Botez, R. M., Grigorie, L., Mamou, M., Mebarki, Y., 2016,Open Loop Morphing Wing Architecture based ANFIS Controller, AIAA Atmospheric Flight Mechanics Conference, Washington, DC, Etats-unis, 13-17 juin.

  3. Murrieta Mendoza, A., Hamy, A., Botez, R. M., 2016,Lateral Reference Trajectory Algorithm Using Ant Colony Optimization, 16th AIAA Aviation Technology, Integration, and Operations Conference, Washington, DC, Etats-unis, 13-17 juin.

  4. Murrieta Mendoza, A., Bunel, A., Botez, R. M., 2016,Aircraft Vertical Reference Trajectory Optimization With a RTA Constraint Using the ABC Algorithm, 16th AIAA Aviation Technology, Integration, and Operations Conference, Washington, DC, Etats-unis, 13-17 juin.

  5. Sugar Gabor O., Koreanschi, A., Botez, R. M., Mamou, M., Mebarki, Y., 2016,Analysis of the Aerodynamic Performance of a Morphing Wing-Tip Demonstrator Using a Novel Nonlinear Vortex Lattice Method, 34th AIAA Applied Aerodynamics Conference, AIAA Aviation, Washington, DC, Etats-unis, 13-17 juin.

  6. Koreanschi, A., Sugar Gabor O., Acotto, J., Botez, R. M., Mamou, M., Mébarki, Y., 2016,A Genetic Algorithm Optimization Method for a Morphing Wing Tip Demonstrator Validated Using Infra-Red Experimental Data, 34th AIAA Applied Aerodynamics Conference, AIAA Aviation, Washington, DC, Etats-unis, 13-17 juin.

  7. Sugar Gabor, O., Koreanschi, A., Botez, R. M., 2016,Aerodynamic Analysis of Upper Surface Wing Morphing Efficiency for the S4 Éhecatl Unmanned Aerial System, 2016 International Conference on Unmanned Aerial Systems ICUAS’16, Arlington, DC, Etats-unis, 7-10 juin.

  8. Tondji, Y., Botez, R., 2016,Numerical-Empirical Estimation and Experimental Validation the Inertial Properties of the Unmanned Aerial System - UAS-S4 of Hydra Technologies, 2016 International Conference on Unmanned Aerial Systems ICUAS’16, Arlington, DC, Etats-unis, 7-10 juin.

  9. Boughari, Y., Ghazi, G., Botez, R. M., 2016,Optimal Control New Methodologies Validation on the Research Aircraft Flight Simulator of the Cessna Citation X Business Aircraft, Book of Abstract, ISBN 978-3-9816624-8-1, Science and Engineering for Reliable Energy, The 6th International Conference & Workshop REMOO-2016, Budva, Montenegro, 18-20 mai.

  10. Tchatchueng Kammegne, M. J., Botez, R. M., Grigorie, T. L., Mamou, M., Mébarki, Y., 2016,Aircraft Energy Consumption Limitation through Drag Reduction based on Morphing Wing Technology – A New Multidisciplinary Experimental Model, Book of Abstract, ISBN 978-3-9816624-8-1, Science and Engineering for Reliable Energy, The 6th International Conference & Workshop REMOO-2016, Budva, Montenegro, 18-20 mai.

  11. Hamy, A., Murrieta-Mendoza, A., Botez, R., 2016,Flight Trajectory Optimization to reduce Fuel Burn and Polluting Emissions using a Performance Database and Ant Colony Optimization Algorithm, AEGATS ‘16 Advanced Aircraft Efficiency in a Global Air Transport System, Paris, France, 12-14 avril.

  12. Tchatchueng Kammegne, M. J., Botez, R. M., Grigorie, T. L., 2016, Actuation Mechanism Control in a Morphing Application with a Full Scaled Portion of an Aircraft Wing, IASTED Modelling, Identification and Control Conference, Innsbruck, Autriche, 16-17 fevrier.

  13. Tchatchueng Kammegne, M. J., Botez, R. M., Mamou, M., Mébarki, Y., Koreanschi, A., Sugar Gabor, O., Grigorie, T. L., 2016, Experimental Wind Tunnel Testing of a New Multidisciplinary Morphing Wing Model, Advances in Mathematics and Computer Science and their Applications (Book title), Series title: Mathematics and Computers in Science and Engineering Series (57), WSEAS Press (www.wseas.org), Proceedings of the 18th International Conference on Mathematical Methods, Computational Techniques and Intelligent System (MAMECTIS ’16), pp. 90-97, Venice, Italy, January 29-31, ISSN: 2227-4588, ISBN: 978-1-61804-360-3.

  14. Grigorie, L. T., Botez, R. M., Popov, A. V., 2016, Self-Adaptive Morphing Wing Model, Smart Actuated and controlled by using a Multi-Loop Controller based on a Laminar Flow Real Time Optimizer, AIAA SciTech 2016, San Diego, CA, 4-8 janvier.

  15. Koreanschi, A., Sugar Gabor, O., Ayrault, T., Botez, R. M., Mamou, M., Mébarki, Y., 2016, Numerical Optimization and Experimental Testing of a Morphing Wing with Aileron System, AIAA SciTech 2016, San Diego, CA, 4-8 janvier.

  16. Murrieta-Mendoza, A., Hamy, A., Botez, R. M., 2015, Mach Number Selection for Cruise Phase Using Ant Colony Algorithm for RTA Constraints, International Conference on Air Transport INAIR 2015, Amsterdam, Pays-Bas, 12-13 novembre.

  17. Ghazi, G., Botez, R. M., Tudor, M., 2015, Identification of a Cessna Citation X Aero-Propulsive Model in Climb Regime from Flight Tests, International Conference on Air Transport INAIR 2015, Amsterdam, Pays-Bas, 12-13 novembre.

  18. Murrieta-Mendoza, A., Bunel, A., Botez, R. M., 2015, Aircraft Lateral Flight Optimization Using Artificial Bees Colony, International Conference on Air Transport INAIR 2015, Amsterdam, Pays-Bas, 12-13 novembre.

  19. Ghazi, G., Rezk, K. G., Botez, R. M., 2015, Cessna Citation X Pitch Rate Control Design using Guardian Maps, International Conference on Air Transport INAIR 2015, Amsterdam, Pays-Bas, 12-13 novembre.

  20. Murrieta-Mendoza, A., Botez, R. M., Patrón, R. S. F., 2015, Flight Altitude Optimization Using Genetic Algorithms considering Climb and Descent Costs in Cruise with Flight Plan Information, SAE 2015 AeroTech Congress & Exhibition, Seattle, WA, États-unis, 22-24 septembre.

  21. Murrieta-Mendoza, A., Botez, R., 2015, Aircraft Vertical Route Optimization Deterministic Algorithm for a Flight Management System, SAE 2015 AeroTech Congress & Exhibition, Seattle, WA, États-unis, 22-24 septembre.

  22. Ghazi, G., Botez, R., 2015, Development of a High-Fidelity Simulation Model for a Research Environment, SAE 2015 AeroTech Congress & Exhibition, Seattle, WA, États-unis, 22-24 septembre.

  23. Ghazi, G., Botez, R. M., Achigui, J. M., 2015, Cessna Citation X Engine Model Identification from Flight Tests, SAE 2015 AeroTech Congress & Exhibition, Seattle, WA, États-unis, 22-24 septembre.

  24. Ghazi, G., Botez, R. M., Tudor, M., 2015, Performance Database Creation for Cessna Citation X Aircraft in Climb Regime using an Aero-Propulsive Model developed from Flight Tests, Sustainability 2015 - An International Conference on Environmental Sustainability in Air Vehicle Design and Operations of Helicopters and Airplanes, Montréal, Qué., Canada, 22-24 septembre.

  25. Murrieta-Mendoza, A., Gagné, J., Botez, R. M., 2015, GRIB2 Weather Extraction and Use for Flight Optimization Algorithms, Sustainability 2015 - An International Conference on Environmental Sustainability in Air Vehicle Design and Operations of Helicopters and Airplanes, Montréal, Qué., Canada, 22-24 septembre.

  26. Murrieta-Mendoza, A., Félix-Patrón, R. S., Botez, R. M., 2015, Genetic Algorithms for Altitude Optimization During Cruise, Sustainability 2015 - An International Conference on Environmental Sustainability in Air Vehicle Design and Operations of Helicopters and Airplanes, Montréal, Qué., Canada, 22-24 septembre.

  27. Sugar Gabor, O., Botez, R. M., Stan, D., 2015, Preliminary Analysis of the Lip Wing System for the ALIPTERA VTOL Concept Aircraft, Sustainability 2015 - An International Conference on Environmental Sustainability in Air Vehicle Design and Operations of Helicopters and Airplanes, Montréal, Qué., Canada, 22-24 septembre.

  28. Anthony, J., Hamel, C., Botez, R. M., 2015, Identification of the Roll Response for the Cessna Citation X Business Aircraft, 39th ARA Congress, Frascati, Italie, 29-31 juillet.

  29. Anthony, J., Hamel, C., Botez, R. M., 2015, Optimization of Engine Model Parameters Gain and Time Constant for the Cessna Citation X Business Aircraft Engine, 39th ARA Congress, Frascati, Italie, 29-31 juillet.

  30. Murrieta Mendoza, A., Beuze, B., Ternisien, L., Botez, R. M., 2015, Branch & Bound-based Algorithm for Aircraft VNAV Profile Trajectory Optimization, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2280, Dallas, Texas, États-Unis, 22-26 juin.

  31. Felix Patron, R. S., Schindler, M., Botez, R. M., 2015, , Aircraft Trajectories Optimization By Genetic Algorithms To Reduce Flight Cost Using A Dynamic Weather Model, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2281, Dallas, Texas, États-Unis, 22-26 juin.

  32. Liv, A., Dancila, R. I., Botez, R. M., 2015, Trajectory optimization algorithm for a constant altitude cruise flight with a required time of arrival constraints, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2259, Dallas, Texas, États-Unis, 22-26 juin.

  33. Sugar Gabor, O., Koreanschi, A., Botez, R. M., 2015, Numerical study of UAS-S4 Éhecatl aerodynamic performance improvement obtained with the use of a morphing wing approach, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2282, Dallas, Texas, États-Unis, 22-26 juin.

  34. Koreanschi, A., Sugar Gabor, O., Botez, R. M., 2015, Numerical and Experimental Validation of a Morphed Wing Geometry Using Price-Païdoussis Wind Tunnel Testing, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-3386, Dallas, Texas, États-Unis, 22-26 juin.

  35. Tchatchueng Kammegne, M. J., Nguyen, D-H., Botez, R. M., Grigorie, T. L., 2015, Control Validation of a Morphing Wing in an Open Loop Architecture, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2499, Dallas, Texas, États-Unis, 22-26 juin.

  36. Khan, S., Botez, R. M., Grigorie, L. T., 2015, A New Method for Tuning PI Gains for Position Control of BLDC Motor Based Wing Morphing Actuators, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2497, Dallas, TX, EUs, 22-26 juin.

  37. Beulze, B., Dancila, B., Botez, R. M., 2015, Presentation of three methods results comparison for Vertical Navigation VNAV trajectory optimization for the Flight Management System FMS, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2597, Dallas, Texas, États-Unis, 22-26 juin.

  38. Gautier, M. M., Dancila, R., Botez, R. M., 2015, Optimization of the Cruise Regime of Flight Airplane Trajectory using Deterministic Algorithms, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-3179, Dallas, Texas, États-Unis, 22-26 juin.

  39. Communier, D., Salinas Flores, M., Carranza Moyao, O., Botez, R. M., 2015, Aero structural modeling of a wing using CATIA V5 and XFLR5 software and experimental validation using the Price-Païdoussis wing tunnel, AIAA Aviation 2015, 15th AIAA Aviation Technology, Integration, and Operation Conference, http://arc.aiaa.org/doi/abs/10.2514/6.2015-2558, Dallas, Texas, États-Unis, 22-26 juin.

  40. Aissaoui, R., Hang, A. L., Carranza Moyao, O., Gerald, P., Botez, R., 2015, Effect of Wind Tunnel Velocity on the Dynamics of Human Walking, 62nd CASI Aeronautics Conference and AGM & 3rd GARDN Conference, Montreal, Que., Canada, 19-21 mai.

  41. Kazubu, J. N., Botez, R. M., Sugar Gabor, O., 2015, Design of UAV-S4 composite morphing wing, 62nd CASI Aeronautics Conference and AGM & 3rd GARDN Conference, Montreal, Que., Canada, 19-21 mai.

  42. Mosbah, A. B., Flores Salinas, M., Ayrault, T., Botez, R., Dao, T. M., 2015, EGD-ANN model to predict actuators displacements for an open loop morphing wing system, 62nd CASI Aeronautics Conference and AGM & 3rd GARDN Conference, Montreal, Que., Canada, 19-21 mai.

  43. Ghazi, G., Botez, R. M., 2015, Lateral Control Design for the Cessna Citation X with Robustness and Handling Qualities, 62nd CASI Aeronautics Conference and AGM & 3rd GARDN Conference, Montreal, Que., Canada, 19-21 mai.

  44. Nguyen, D. H., Khan, S., Tchatchueng Kammegne, M. J., Botez, R. M., 2015, A Predictive PID Controller Design for an Actuator attached inside a Morphing Wing, 62nd CASI Aeronautics Conference and AGM & 3rd GARDN Conference, Montreal, Que., Canada, 19-21 mai.

  45. Botez, R. M., 2015, Level D Research Aircraft Flight Simulator use for Novel Methodologies in Aircraft Modeling and Simulation, 3rd International Workshop on Numerical Modelling in Aerospace Sciences NMAS 2015, Bucarest, Roumanie.

  46. Murrieta-Mendoza, A., Demange, S., George, F., Botez, R., 2015, Performance Database Creation using a Level D Simulator for Aircraft Trajectory Optimization, IASTED Modeling, Simulation and Control conference, Innsbruck, Autriche, 16-17 février.

  47. Tchatchueng Kammegne, M. J., Belhadj, H., Nguyen, D-H., Botez, R. M., 2015, Nonlinear Control Logic for an Actuator to Morph a Wing: Design and Experimental Validation, IASTED Modeling, Simulation and Control conference, Innsbruck, Autriche, 16-17 février.

  48. Tchatchueng Kammegne, J., Khan, S., Botez, R. M., 2015, New Methodology for the Controller of an Electrical Actuator for Morphing a Wing, The 23nd AIAA/ASME/AHS Adaptive Structures Conference, American Institute of Aeronautics and Astronautics AIAA Science and Technology Forum 2015, Kissimee, Floride, États- Unis, 5-9 janvier.

  49. Vincent, J. B., Botez, R. M., 2015, Systemic Modeling and Design Approach for Morphing Wing Aileron Controller using Matlab/Simulink, The 23nd AIAA/ASME/AHS Adaptive Structures Conference, American Institute of Aeronautics and Astronautics AIAA Science and Technology Forum 2015, Kissimee, Floride, États-Unis, 5-9 janvier.

  50. Şugar Gabor, O., Koreanschi, A., Botez, R. M., 2014, Numerical Study of UAS-S4 Ehécatl Aerodynamic Performance Improvement using a Morphing Wing Technology, Unmanned Systems Canada 2014 Annual Conference, Montréal, Qué., Canada, 4-6 novembre.

  51. Şugar Gabor, O., Simon, A., Koreanschi, A., Botez, R. M., 2014, Application of a Morphing Wing Technology on Hydra Technologies Unmanned Aerial System UAS-S4, The ASME 2014 International Mechanical Engineering Congress & Exposition, Montréal, Que., Canada, 14-20 novembre.

  52. Murrieta Mendoza, A., Botez, R. M., 2014, Lateral Navigation Optimization Considering Winds and Temperatures for Fixed Altitude Cruise using the Dijsktra’s Algorithm, The ASME 2014 International Mechanical Engineering Congress & Exposition, Montréal, Que., Canada, 14-20 novembre.

  53. Mosbah, A. B., Botez, R. M., Dao, T. M., 2014, New Methodology for the Calculation of Aerodynamic Coefficients on ATR-42 Scaled Model with Neural Network-EGD Method, The ASME 2014 International Mechanical Engineering Congress & Exposition, Montréal, Que., Canada, 14-20 novembre.

  54. Felix Patron, R. S., Botez, R, M., 2014, Flight Trajectory Optimization through Genetic Algorithms Coupling Vertical and Lateral Profiles, The ASME 2014 International Mechanical Engineering Congress & Exposition, Montréal, Que., Canada, 14-20 novembre.

  55. Murrieta Mendoza, A., Botez, R. M., 2014, Method to calculate an Aircraft VNAV Trajectory Cost using a Performance Database, The ASME 2014 International Mechanical Engineering Congress & Exposition, Montréal, Que., Canada, 14-20 novembre.

  56. Tondji Chendjou, Y. W., Botez, R. M., 2014, Numerical and Experimental Measures of the Unmanned Aerial System UAS-S4 of Hydra Technologies, SAE 2014 Aerospace Systems and Technology Conference, Cincinnati, Ohio, États-Unis, 23-25 septembre.

  57. Hamel, C., Botez, R. M., Ruby, M., 2014, Cessna Citation X Airplane Grey-Box Model Identification without Preliminary Data, SAE 2014 Aerospace Systems and Technology Conference, Cincinnati, Ohio, États-Unis, 23-25 septembre.

  58. Mosbah, A. B., Botez, R. M., Dao, T. M., 2014, New Methodology for the Prediction of the Aerodynamic Coefficients of an ATR-42 Scaled Wing Model, SAE 2014 Aerospace Systems and Technology Conference, Ohio, États-Unis, 23-25 septembre.

  59. Boughari, Y., Botez, R. M., Ghazi, G., Theel, F., 2014, Evolutionary Algorithms for Robust Cessna Citation X Flight Control, SAE 2014 Aerospace Systems and Technology Conference, Cincinnati, Ohio, États-Unis, 23-25 septembre.

  60. Sugar Gabor, O., Simon, A., Koreanschi, A., Botez, R., 2014, Numerical Optimization of the UAS-S4 Éhecatl Morphing Airfoil, AIAA’s Aviation 2014, Atlanta, Géorgie, États-Unis, 16-20 juin.

  61. Koreanschi, A., Gabor Sugar, O., Botez, R. M., 2014, Boundary Layer Behavior on Morphing Upper Surface Wings with Shape Changing Aileron - New Analysis Techniques, AIAA’s Aviation 2014, Atlanta, Géorgie, États-Unis, 16-20 juin.

  62. Murrieta Mendoza, A., Botez, R. M., Labour, D., 2014, Navigation Trajectory Optimization Algorithm for the FMS CMA-9000, AIAA’s Aviation 2014, Atlanta, Géorgie, États-Unis, 16-20 juin.

  63. Grigorie, T. L., Popov, A. V., Botez, R. M., 2014, Control Strategies for an Experimental Morphing Wing Model, AIAA’s Aviation 2014, Atlanta, Géorgie, États-Unis, 16-20 juin.

  64. Patron Felix, R. S., Berrou, Y., Botez, R. M., 2014, Climb, Cruise and Descent 3D Trajectory Optimization Algorithm for the FMS CMA-9000 on the Airbus A310, AIAA’s Aviation 2014, Atlanta, Géorgie, États-Unis, 16-20 juin.

  65. Dancila, B. D., Botez, R. M., 2014, Construction of an Aircraft's VNAV Flight Envelope for in-FMS Flight Trajectory Computation and Optimization: Application on the Airbus A310 Performance Data, AIAA’s Aviation 2014, Atlanta, Géorgie, États-Unis, 16-20 juin.

  66. Grigorie, L. T., Sandu, D. G., Botez, R. M., 2014, A Redundant Aircraft Attitude System Based on Fuzzy Logic Data Fusion of the Miniaturized Inertial Sensors, AHS 70th Annual Forum & Technology Display, Montréal, Qué., Canada, May 20-22.

  67. Ghazi, G., Botez, R. M., 2014, New Robust Control Analysis Methodology for Lynx Helicopter and Cessna Citation X Aircraft Using Guardian Maps, Genetic Algorithms and LQR Theories Combinations, AHS 70th Annual Forum & Technology Display, Montréal, Qué., Canada, 20-22 mai.

  68. Murrieta, A., Botez, R. M., Ford, S., 2014, Estimation of fuel consumption and polluting emissions generated during the missed approach procedure, IASTED Modeling, Simulation and Control conference, Innsbruck, Autriche, 17-19 février.

  69. Kammegne Tchatchueng, M. J., Grigorie, L. T., Botez, R. M., Koreanschi, A., 2014, Design and validation of a position controller in the Price-Païdoussis wind tunnel, IASTED Modeling, Simulation and Control conference, Innsbruck, Autriche, 17-19 février.

  70. Boughari, Y., Botez, R. M., Theel, F., Ghazi, G., 2014, Optimal flight control on Cessna Citation X aircraft using Differential Evolution, IASTED Modeling, Simulation and Control conference, Innsbruck, Autriche, 17-19 février.

  71. Grigorie. L.T., Jula, N., Negrea, R., Obreja, R., Botez, R. M., 2014, Optimization of a smart accelerometer based on amplitude-frequency characteristics constraints, IASTED Modeling, Simulation and Control conference, Innsbruck, Autriche, 17-19 février.

  72. Grigorie, L. T., Botez, R. M., Sandu, D. G., 2014, Experimental testing of a data fusion algorithm for miniaturized sensors in redundant configurations, MMSSE 2014, The 2014 International Conference on Mathematical Methods, Mathematical Models and Simulation in Science and Engineering, Interlaken, Suisse, 20-22 février.

  73. Botez, R. M., 2014, New controller design and experimental validation using wind tunnel tests for a morphing wing, Greener Aviation Clean Sky breakthroughs and worldwide status, Brussels, Belgique, 12-14 mars.

  74. Botez, R. M., 2014, Optimization of aircraft flight trajectories for Flight Management System, Greener Aviation Clean Sky breakthroughs and worldwide status, Brussels, Belgique, 12-14 mars.

  75. Patron, R. F., Botez, R. M., Labour, D., 2013, Optimized cruise in the presence of winds for the FMS CMA-9000 using genetic algorithms, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  76. Patron, R. F., Botez, R. M., Labour, D., 2013, Optimized climb for the FMS CMA-9000 using genetic algorithms, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  77. Sidibe, S., Botez, R. M., 2013, Trajectory optimization of FMS-CMA 9000 by dynamic programming, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  78. Gabor Sugar, O., Koreanschi, A., Botez, R. M., 2013, An efficient numerical lifting line method for practical wing optimization through morphing on the Hydra Technologies UAS-S4, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  79. Hassig, A., Brossard, J., Botez, R. M., 2013, Calibration issues in the Subsonic Price - Païdoussis Wind Tunnel, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  80. Mosbah, A. B., Botez, R. M., Dao, T.M., 2013, New methodology for calculating flight parameters with neural network – EGD method, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  81. Boughari, Y., Ghazi, G., Theel, F., Botez, R. M., 2013, Business aircraft flight control system using robust H-infinity controllers on Cessna Citation X, CASI AÉRO 2013 conference, Toronto, Ontario, Canada, 30 avril - 2 mai.

  82. Fays, J., Botez, R. M., 2013, Aircraft trajectories generation by use of No Fly Zones self management for a Flight Management System, 15th Australian International Aerospace Congress, Melbourne, Australie, 25-28 février

  83. Michaud, F., Joncas, S., Botez, R. M., 2013, Design, Manufacturing and Testing of a Small-Scale Composite Morphing Wing, 19th International Conference on Composite Materials, Montréal, Québec, Canada, 28 juillet - 2 août

  84. Gagné, J., Murrieta, A., Botez, R. M., Labour, D., 2013, New method for aircraft fuel saving using Flight Management System and its validation on the L-1011 aircraft, 2013 Aviation Technology, Integration, and Operations (ATIO) Conference and International Powered Lift Conference (IPLC), Los Angeles, CA, Etats-unis, 12-14 août

  85. Patron, R. F., Botez, R. M., Labour, D., 2013, Speed and altitude optimization on the FMS CMA-9000 for the Sukhoi Superjet 100 using genetic algorithms, 2013 Aviation Technology, Integration, and Operations (ATIO) Conference and International Powered Lift Conference (IPLC), Los Angeles, Californie, États-Unis, 12-14 août

  86. Patron, R. F., Botez, R. M., Labour, D., 2013, Low calculation time interpolation method on the altitude optimization algorithm for the FMS CMA-9000 improvement on the A-310 and L-1011 aircraft, 2013 Aviation Technology, Integration, and Operations (ATIO) Conference and International Powered Lift Conference (IPLC), Los Angeles, Californie, États-Unis, 12-14 août

  87. Dancila, R., Botez, R. M., Ford, S., 2013, Fuel burn and emissions evaluation for a missed approach procedure performed by a B737-400, 2013 Aviation Technology, Integration, and Operations (ATIO) Conference and International Powered Lift Conference (IPLC), Los Angeles, Californie, États-Unis, 12-14 août

  88. Patron, R. F., Kessaci, A., Botez, R. M., Labour, D., 2013, Flight trajectories optimization under the influence of winds using genetic algorithms, AIAA Guidance, Navigation, and Control Conference, Boston, Massachusetts, Etats-unis, 19-22 août

  89. Mosbah, A. B., Botez, R. M., Dao, T.M., 2013, New methodology for calculating flight parameters with neural network – Extended Great Deluge method applied on a reduced scale wind tunnel model of an ATR-42 wing, AIAA Guidance, Navigation, and Control Conference, Boston, Massachusetts, Etats-unis, 19-22 août

  90. Grigorie, L.T., Popov, A. V., Botez, R. M., 2013, Control of Actuation System Based Smart Material Actuators in a Morphing Wing Experimental Model, Invited paper, AIAA Guidance, Navigation, and Control Conference, Boston, Massachusetts, Etats-unis, 19-22 août

  91. Şugar Gabor, O., Koreanschi, A., Botez, R. M., 2013, Unmanned Aerial System Hydra Technologies Éhecatl wing optimization using a morphing approach, AIAA Guidance, Navigation, and Control Conference, Boston, Massachusetts, Etats-unis, 19-22 août

  92. Grigorie, T. L., Botez, R. M., 2013, Redundant Inertial Navigator for Robotic Applications, ICINCO 2013, Reykjavik, Islande, 29-31 juillet

  93. Grigorie, T. L., Botez, R. M., 2013, A redundant aircraft attitude system based on miniaturized gyro clusters data fusion, EUROCON 2013, Zagreb, Croatie, 1-4 juillet

  94. Cauzard, V., Simon, A., Botez, R. M., 2013, Aerodynamics simulation of the Hydra Technologies Unmanned Aerial System UAS S4 using the Fluent Code, SAE Technical Paper 2013-01-2267, 2013, doi:10.4271/2013-01-2267, SAE AeroTech Congress & Exhibition 2013, Montréal, Québec, Canada, 24-26 septembre

  95. Hamel, C., Sassi, A., Botez, R. M., Dartigues, C., 2013, Cessna Citation X aircraft global model identification from fight tests, SAE AeroTech Congress & Exhibition 2013, Montréal, Québec, Canada, 24-26 septembre

  96. Sugar Gabor, O., Koreanschi, A., and Botez, R. M., 2013, Optimization of an Unmanned Aerial System' Wing Using a Flexible Skin Morphing Wing, SAE AeroTech Congress & Exhibition 2013, Montréal, Québec, Canada, 24-26 septembre

  97. Ben Mosbah, A., Flores Salinas, M., Botez, R. M., and Dao, T., 2013, New Methodology for Wind Tunnel Calibration Using Neural Networks - EGD Approach, SAE AeroTech Congress & Exhibition 2013, Montréal, Québec, Canada, 24-26 septembre

  98. Rodriguez Fajardo, L., Botez, R. M., 2012, Civil turbofan engines semi-empirical thrust generic model, IECON 2012 conférence, Montréal, Québec, Canada, 25-28 octobre

  99. Sugar Gabor, O., Koreanschi, A., Botez, R. M., 2012, Low-speed aerodynamic characteristics improvement of ATR 42 airfoil using a morphing wing approach, IECON 2012 conférence, Montréal, Québec, Canada, 25-28 octobre

  100. Patron Felix R., Botez R.M., Labour, D., 2012, Vertical profile optimization for the Flight Management System CMA-9000 using the golden section search method, IECON 2012 conférence, Montréal, Québec, Canada, 25-28 octobre

  101. Grigorie, L. T., Botez, R. M., Edu, I. R., Corcau, J., 2012, Bi-dimensional SDINS in horizontal plane with miniaturized redundant IMU, IECON 2012 conférence, Montréal, Québec, Canada, 25-28 octobre

  102. Boughari, Y., Botez, R. M., 2012, Optimal flight control on the Hawker 800 XP business aircraft, IECON 2012 conférence, Montréal, Québec, Canada, 25-28 octobre

  103. Dancila, B. D., Botez, R.M., Labour, D., 2012, Fuel burn prediction algorithm for cruise, constant speed and level flight segments.AIAA Guidance, Navigation and Control conference, Minneapolis, MI, Etats-unis, 13-17 août.

  104. Vincent, J-B, Botez, R.M., Popescu, D., Ghazi, G.,, 2012, A new methodology for a business aircraft model Hawker 800 XP stability analysis using Presagis FLSIM, AIAA Guidance, Navigation and Control conference, Minneapolis, MI, Etats-unis, 13-17 août.

  105. Grigorie, L. T., Botez, R. M., Popov, A.-V., 2012, Design and experimental validation of a control system for a morphing wing, AIAA Atmospheric Flight Mechanics conference, Invited session paper, Minneapolis, MI, États-unis, 13-17 août.

  106. Fajardo, L., Botez, R.M., 2012, Generic new modelling technique for turbofan engines thrust, AIAA Modelling and Simulation Technologies conference, Minneapolis, MI, Etats-unis, 13-17 août.

  107. Anton, N., Botez, R., Weight functions method for stability analysis: applications and experimental validation for Hawker 800XP aircraft, AIAA Modelling and Simulation Technologies conference, Minneapolis, MI, Etats-unis, 13-17 août.

  108. Silisteanu, P.D., Botez, R. M., 2012, Two-dimensional airfoil shape optimization for airfoils at low speeds,, AIAA Atmospheric Flight Mechanics conference, Invited session paper, Minneapolis, MI, Etats-unis, 13-17 août.

  109. Grigorie, L.T., Botez, R.M., Sandu, D. G., Obreja, R, 2012, A redundant bi-dimensional inertial navigator in veritcal plane, 16th WSEAS International Conference on Systems (part of CSCC`12), Kos, Grèce, 14-16 juillet.

  110. Grigorie, L.T., Edu, I. R., Obreja, R., Botez, R. M., 2012, A numerical implemented method for the aircraft attitude determination, Naples, Italie, 25-27 juin.

  111. Anton, N., Botez, R. M., 2012, Aircraft X-31 stability analysis and validation with experimental data, Naples, Italie, 25-27 juin.

  112. Grigorie, L.T., Edu, I. R., Obreja, R., Botez, R. M., 2012, An attitude software tool based on a matrix method, The 36th ARA Congress - Learning without frontiers, Bari, Italie, 29 mai-3 juin.

  113. Grigorie, L. T., Botez, R. M., Popov, A. V., Mamou, M.,  Mébarki, Y., 2011, Intelligent control of smart actuators in a new closed loop morphing wing mechanism, ICAST  - The 22nd International Conference on Adaptive Structures Technologies, Corfu, Grèce, 10-12 octobre.

  114. Anton, N., Botez, R. M., 2011, A new type of the stability derivatives for X-31 model aircraft validated using wind tunnel test data, Applied Vehicle Technology Panel Specialists Meeting AVT-189,  Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles,  Dstl Portsdown West, Fareham, Hampshire, Grande Bretagne, 12-14 octobre.

  115. Grigorie, L. T., Popov, A. V., Botez, R. M., Mamou, M.,  Mébarki, Y., 2011, Smart concepts for actuation system and its control in a morphing wing, 13th National Conference Caius Iacob in Fluid Mechanics and Technological Applications, INCAS, Bucharest, Roumanie, 29-30 septembre. 

  116. Grigorie, L.T., Botez, R. M., Popov, A.V., Mamou, M., Mébarki, Y., 2011, A new morphing mechanism for a wing using smart actuators controlled by a self-tuning fuzzy logic controller, AIAA Centennial of Naval Aviation Forum: 100 Years of Achievement and Progress, Virginia Beach, VA, Etats-unis, 20-22 septembre.

  117. Grigorie, L.T., Popov, A.V., Botez, R. M., Mamou, M., Mébarki, Y., 2011, Controller and Aeroelasticity Analysis for a Morphing Wing, Session for Invited Papers: Aircraft Aeroservoelastic Control, Modeling, Simulation and Optimization, AIAA Atmospheric Flight Mechanics Conference, Portland, Etats-unis, 8-11 août.

  118. Grigorie, L. T., Botez, R. M., 2011, Miniaturized inertial sensors’ noise reduction by using redundant linear configurations, IASTED conference in Applied Simulation and Modeling, Crète, Grèce, 22-24 juin.

  119. Grigorie, L. T., Popov, A. V., Botez, R. M., Mamou, M.,  Mébarki, Y., 2011, Intelligent control of a morphing wing, Part 1: Design phase, The 19th IASTED conference in Applied Simulation and Modeling, Crète, Grèce, 22-24 juin.

  120. Grigorie, L. T., Popov, A. V., Botez, R. M., Mamou, M.,  Mébarki, Y., 2011, Intelligent control of a morphing wing, Part 1: Validation phase, IASTED conference in Applied Simulation and Modeling, Crète, Grèce, 22-24 juin.

  121. Langlet, B., Salameh, T., Botez, R. M., Labour, D., 2011, FMS optimization and climb during cruise regime, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  122. Dancila, B., Botez, R.M., Labour, D., 2011, Altitude optimization algorithm for cruise, constant speed, level flight segments, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  123. Fays, J., Botez, R.M., 2011, Generation and following of 4D trajectories for an aircraft, using no Fly Zones self-management for a flight management system application, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  124. Grigorie, L.T., Obreja, R., Botez, R.M., Sandu, D., 2011, Error model of a bidimensional SDINS in vertical plane, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  125. Pollender-Moreau, O., Botez, R.M., 2011, Practical sequencing method between aerodynamic modeling using the Vortex Lattice Method and a simulation platform for an autopilot using optimal control techniques, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  126. Grigorie, L.T., Botez, R. M., Popov, A.V., Mamou, M., Mébarki, Y., 2011, Application of a bidimensional SDINS in vertical plane, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  127. Silisteanu, P., Botez, R.M., 2011, Fast procedure for two dimensional airfoil design, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  128. Anton, N., Botez, R.M., 2011, The weight function method and its application to the mid-size Hawker 800 XP corporate aircraft, Canadian Aeronautics and Space Institute AÉRO 11, 58th Aeronautics Conference and AGM, Montréal, Québec, Canada, 26-28 avril.

  129. Grigorie, L.T., Botez, R. M., Popov, A.V., Mamou, M., Mébarki, Y., 2011, A hybrid fuzzy logic proportional integral derivative plus conventional on-off controller for a morphing wing actuation using shape memory alloys, AIAA-SDM 2011, Denver, Colorado, Etats-unis, 4-7 avril.

  130. Popov, A.-V., Grigorie, L. T., Botez, R. M., Mamou, M., Mebarki, Y., 2010, Morphing Wing Real Time Optimization in Wind Tunnel Tests, The International Conference on Informatics in Control, Automation and Robotics ICINCO 2010, Madeira, Portugal, 15-18 juin.

  131. Boely, N., Botez, R. M., 2010, New Methodologies for the Identification and Validation of a Nonlinear F/A-18 Model by use of Neural Networks, Session pour des papiers invités: Aircraft Aeroservoelastic Control, Modeling, Simulation, and Optimization, AIAA Atmospheric Flight Mechanics Conference, Toronto, Ontario, Canada, 2-5 aout.

  132. Silisteanu, P., Botez, R.M., 2010, New Fourth Order Code for the Three Dimensional Integration of the Euler System of Equations, The Royal Aeronautical Society RAeS Aerodynamics Conference, Bristol, Grande Bretagne, 27-28 juillet

  133. Popov, A.-V., Grigorie, L. T., Botez, R. M., Mamou, M., Mebarki, Y., 2010, Morphing Wing Real Time Optimization in Wind Tunnel Tests, The International Conference on Informatics in Control, Automation and Robotics ICINCO 2010, Madeira, Portugal, 15-18 juin.

  134. Grigorie, L. T., Popov, A.-V., Botez, R. M., Mamou, M., Mebarki, Y., 2010, A Morphing Wing Used Shape Memory Alloy Actuators New Control Technique with Bi-Positional and PI Laws Optimum Combination Wind – Part 1: Design Phase, The International Conference on Informatics in Control, Automation and Robotics ICINCO 2010, Madeira, Portugal, 15-18 juin.

  135. Grigorie, L. T., Popov, A.-V., Botez, R. M., Mamou, M., Mebarki, Y., 2010, A Morphing Wing Used Shape Memory Alloy Actuators New Control Technique with Bi-Positional and PI Laws Optimum Combination Wind – Part 2: Experimental Validation, The International Conference on Informatics in Control, Automation and Robotics ICINCO 2010, Madeira, Portugal, 15-18 juin.

  136. Popov, A.-V., Grigorie, L. T., Botez, R. M., Mamou, M., Mebarki, Y., 2010, Controller Optimization in Real Time for a Morphing Wing in a Wind Tunnel, The 15th IEEE Mediterranean Electrotechnical Conference, Malta, 26-28 avril.

  137. Grigorie, L. T., Botez, R. M., 2010, Adaptive Neuro-Fuzzy Inference Controllers for Smart Material Actuators, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Orlando, Floride, États-Unis, 12-15 avril.

  138. Grigorie, L. T., Botez, R. M., 2010, Neuro-Fuzzy Controller for SMAs for a Morphing Wing Application, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Orlando, Floride, États-Unis, 12-15 avril.

  139. Courchesne, S., Popov, A.-V., Botez, R. M., 2010, New Aeroelastic studies for a morphing wing, 48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Floride, États-Unis, 7-10 janvier.

  140. Silisteanu, P.-D., Botez, R. M., 2010, Transition flow occurrence estimation new method, 48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Floride, États-Unis, 7-10 janvier.

  141. Popov, A.-V., Grigorie, L. T., Botez, R. M., 2009, Morphing wing control validation   during bench tests, IASTED Identification, Control and Applications ICA Conference, Honolulu, Hawaii, États-Unis,17-19 août.

  142. Grigorie, L. T., Popov, A.-V., Botez, R. M., Mamou, M., Mebarki, Y., 2009, Modeling and testing of a morphing wing in open loop architecture, IASTED Modeling and Simulation Conference, Honolulu, Hawaii, États-Unis, 17-19 août.

  143. Gobeault, J., Botez, R.M., Triandaf, I., 2009, Methods of modelling of an underwater unmanned vehicle, AIAA Guidance, Navigation, and Control Conference, Chicago, IL, États-Unis, 10-13 août.

  144. De Jesus Mota, S., Botez, R.M., 2009, New identification method based on neural network for helicopters from flight test data, AIAA Atmospheric Flight Mechanics Conference, Chicago, IL, États-Unis, 10-13 août.

  145. Popov, A.-V., Botez, R.M., Mamou, M., 2009, Temperature variation of optical sensors on a wing during wind tunnel tests, AIAA Guidance, Navigation, and Control Conference, Chicago, IL, États-Unis, 10-13 août.

  146. Grigorie, T.L., Botez, R.M., Popov, A.-V., 2009, Adaptive neuro-fuzzy controllers for an open loop morphing wing system, AIAA Guidance, Navigation, and Control Conference, Chicago, IL, États-Unis, États-Unis, 10-13 août.  

  147. Anton, N., Botez, R.M., Popescu, D., 2009, New methods and code for aircraft stability derivatives calculations from its geometrical data, AIAA Atmospheric Flight Mechanics Conference, Chicago, IL, États-Unis, 10-13 août.

  148. Hidee, A., Botez, R.M., Boely, N., Controls of the F/A-18 AAW based on flight flutter test data, AIAA Guidance, Navigation, and Control Conference, Chicago, IL, États-Unis, 10-13 août.

  149. Anton, N., Botez, R.M., Popescu, D., 2009, New methods and code for aircraft stability derivatives calculations from its geometrical data, CASI Aircraft Design and Development Symposium, Kanata, Ontario, Canada, 5-7 may.

  150. Gobeault, J., Botez, R.M., Triandaf, I., 2009, Modelling and simulation methods of an underwater unmanned vehicle, CASI Aircraft Design and Development Symposium, Kanata, Ontario, Canada, 5-7 may.

  151. Popov, A.-V., Grigorie, L. T., Botez, R. M., 2009, Control of a morphing wing in bench tests, CASI Aircraft Design and Development Symposium, Kanata, Ontario, Canada, 5-7 may.

  152. Silisteanu, P, Botez, R.M., 2009, New methods for transition studies, CASI Aerodynamics Symposium, Kanata, Ontario, Canada, 5-7 may.

  153. Popov, A.-V., Botez, R.M., Mamou, M., Mebarki, Y., Jahrhaus, B., Khalid. M., Grigorie, T.L., 2009, Drag reduction by improving laminar flows past morphing configurations, AVT-168 NATO Symposium on the Morphing Vehicles, Evora, Portugal, 20-23 avril.

  154. Botez, R.M., Grigorie, L. T., Popov, A.-V., 2009, Laminar to turbulent flow transition control on a morphing wing equipped with smart actuators and optical sensors, AVT-168 NATO Symposium on the Morphing Vehicles, Evora, Portugal, 20-23 avril.

  155. Nadeau-Beaulieu, M., Botez, R. M., 2009,  Helicopter main and tail rotor prediction and engine parameters prediction from flight test data, 7th Australian Pacific Vertiflite Conference on Helicopter Technology AIAC, Melboune, Australie, 9-12 mars.

  156. Boely, N., Botez, R., Kouba, G.,  2009, Identification of an F/A-18 nonlinear model between control and structural deflections, 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, États-Unis, 5-8 janvier.

  157. Kouba, G., Botez, R., Boely, N., 2009, Identification of F/A-18 model from flight tests using the fuzzy logic method, 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, États-Unis, 5-8 janvier.

  158. Labib, M., Popov, A-V., Fays, J., Botez, R. M., 2008, Transition point displacement control on a wing equipped with actuators, AIAA Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, États-Unis, 18-21 août.

  159. Botez, R.M., Cotoi, I., 2008, Aerodynamic force optimization for aircraft, EngOpt 2008 International Conference on Engineering Optimization, Rio de Janeiro, Brazil, 1-5 juin.

  160. Botez,  R.M., Grigorie, L. T., Hiliuta, A., 2008, Analytical and simulation method validation for flutter aeroservoelasticity studies,  AVT-156 Advanced Aeroelasticity NATO Meeting, Loen, Norvège, 5-9 mai.

  161. Nadeau Beaulieu, M., Botez, R. M., 2008, Simulation and prediction of main rotor, tail rotor and engine parameters from flight tests, 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Shaumburg, IL, États-Unis, 7-11 avril.

  162. Grigorie, T. L., Botez, R. M., 2007, Neuro fuzzy techniques for an accelerometer bias temperature dependence estimation and compensation, International Conference on Avionics Systems ICAS, Hyderabad, Inde, 20-23 février.

  163. Botez, R. M., Rotaru, M., 2007, Analysis of flying qualities for an F/A-18 aircraft, IASTED International Conference on Applied Simulation and Modeling (ASM 2007), Palma de Majorque, Espagne, 29-31 août.

  164. De Jesus Mota, S., Nadeau Beaulieu, M., Botez, R.M., Brenner, M., 2007, Modeling of structural deflections on a F/A-18 aircraft following flight flutter tests by use of the subspace method, AIAA Guidance, Navigation and Control Conference and Exhibit, Hilton Head, SC, États-Unis, 20-23 août 2007 (Session invitee).

  165. Nadeau Beaulieu, M., De Jesus Mota, S., Botez, R. M., 2007, Flight model identification of an F/A-18 from flight tests, 17th IFAC Symposium on Automatic Control in Aerospace (ACA 2007), Toulouse, France, 25-29 juin.

  166. De Jesus Mota S., Nadeau-Beaulieu, M., Botez, R.M., Subspace method for an F/A-18 aircraft model identification from flight tests, International Forum on Aeroelasticity and Structural Dynamics IFASD 2007, Stockholm, Suède, 18-21 juin.

  167. Biskri, D.E., Botez, R.M., 2007, Method for aerodynamic forces optimizations based on an analytical error formulation,The 7th World Congress on Structural and Multidisciplinary Optimization, Seoul, Corée, 21-25 mai.

  168. Labib, M., Botez, R.M., Popov, A., 2007, Method for the transition point detection from the pressure coefficients distribution, CASI Aircraft Design and Development Symposium, Toronto, Ontario, Canada, 25-26 avril.

  169. Birla, L., 2007, CFD analysis by use of XFoil and Fluent and comparison with wind tunnel test data, CASI Aircraft Design and Development Symposium, Toronto, Ontario, Canada, 25-26 avril.

  170. Botez, R. M., Molaret, P., Laurendeau, E., 2007, Laminar Flow Control on a Research Wing Project Presentation Covering a Three Year Period, CASI Aircraft Design and Development Symposium, Toronto, Ontario, Canada, 25-26 avril.

  171. Botez, R.M., Rotaru, M., 2007, Relationships between flying qualities and flight test parameters for the F/A-18 aircraft, CASI Aircraft Design and Development Symposium, Toronto, Ontario, Canada, 25-26 avril.

  172. Nadeau Beaulieu, M., De Jesus Mota, S., Botez, R. M., 2007, Identification of structural surface deflections on an F/A-18 aircraft using the subspace identification method from flight flutter tests, CASI Aircraft Design and Development Symposium, Toronto, Ontario, Canada, 25-26 avril.

  173. Botez, R.M., Fayard, B., Alban, B., Dionne, P., Mamert, A., Popescu, D., 2007, Stability derivatives calculations and integrations on an aircraft flight model, 12th  Australian International Aerospace Conference, Melbourne, Australie, 20-22 mars.

  174. Botez, R.M., Hiliuta, A., Grigorie, L., 2007, Simulation method for rigid and control modes aeroservoelastic interactions, IASTED International Conference on Modelling, Identification, and Control (MIC 2007),  Insbruck, Autriche, 12-14 février.

  175. Nadeau Beaulieu, M., Botez, R. M., Hiliuta, A., Popov, A-V., 2006, Ground dynamics model validation by use of landing flight test data, AIAA Modeling and Simulation Technologies Conference and Exhibit, Keystone, Colorado, États-Unis, 21-24 août.

  176. Biskri, D.E., Botez, R.M., 2006, Aerodynamic forces approximations calculated with a new   analytical formulation, ASME PVP 2006/ICPVT-11 Conference, Vancouver, CB, Canada, 23-27 juillet.

  177. Botez, R.M., Biskri, D.E., 2006, Simulation method based on analytical error correction for aeroservoelastic interactions studies on an F/A-18 aircraft, The IASTED International Conference on Applied Simulation and Modeling ASM, Rhodes, Grèce, 26-28 juin.

  178. Nadeau-Beaulieu, M., Botez, R. M., Hiliuta, A., Popov, A., Ground dynamics model validation for a simulator certification, International Symposium on Industrial Electronics IEEE_ISIE 2006, Montréal, Québec, Canada, 9-13 juin.

  179. Botez, R.M., Dinu, A. D., Cotoi, I., 2006, Optimisation of unsteady aerodynamic forces for aircraft aeroservoelastic studies, ECCM-2006, 3rd European Conference on Computational Mechanics, Solids, Structures and Coupled Problems in Engineering, Lisbon, Portugal, 5-9 juin.

  180. Hiliuta, A., Botez, R. M., 2006, New Technique for the Aircraft Flight Model Estimation Based on Flight Test Data, Paper AIAA-2006-3482, 36th AIAA Fluid Dynamics Conference and Exhibit, San Francisco, California, États-Unis, 5-8 juin.

  181. Botez, R. M., Dinu, A., Cotoi, I., Stathopoulos, N., Dickinson, M., Terrien, S., Rathé, A., 2006, Aeroservoelasticity Interactions Studies on a Business Aircraft, 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, Rhode Island, États-Unis, 1-4 mai.

  182. Botez, R. M., Dinu, A., Cotoi, I., 2006, Approximations of unsteady aerodynamic forces for closed loop flutter aeroservoelasticity studies, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, États-Unis, 9-12 janvier.

  183. Botez, R.M., Biskri, D.E., Terrien, S., Rathé, A., Stathopoulos, N., Dickinson, M., 2005, Method based on the LS approach used for flutter aeroservoelasticity analysis studies, IASTED MSO Conference, Oranjenstad, Aruba, 29-31 août.

  184. Botez, R., 2005,  New method for aeroservoelastic interactions studies, The 30th Annual ARA Congress, Chisinau, Moldavie, 5-10 juillet, pp. 497-501, ISBN 9975-75-313-2.

  185. Botez, R. M., Biskri, D.E.,  Therien, S., Rathe, A., Stathopoulos, N., Dickinson, M., 2005, New mixed method for unsteady aerodynamic forces approximations for aeroservoelasticity studies,IFASD 2005 – Forum on Aeroelasticity and Structural Dynamics 2005, Munich, Allemagne, 28 juin - 1 juillet.

  186. Biskri, D.E.,  Botez, R.M., Therien, S., Rathe, A., Stathopoulos, N., Dickinson, M.,2005, Mixed method for unsteady aerodynamic forces approximations for aeroservoelasticity studies on fly-by-wire aircraft, Canadian Aeronautical Society  Institute CASI Conference, Toronto, Ontario, Canada, 26-27 avril.

  187. Botez, R. M., Lefebvre, M., 2005, Reduced frequencies ranges selection for unsteady aerodynamic forces in aeroservoelasticity studies on a Fly-by-Wire aircraft, Canadian Aeronautical Society Institute CASI Conference, Toronto, Ontario, Canada, 26-27 avril.

  188. Hiliuta, A., Botez, R.M., 2005, Approximation of unsteady aerodynamic forces by use of combination of fuzzy clustering and shape preserving techniques, Le 20e Congrès Canadien de Mécanique Appliquée, à l’Université McGill, Montréal, Québec, Canada, 30 mai - 2 juin.

  189. Biskri, D.E.,  Botez, R.M., Therien, S., Rathe, A., Stathopoulos, N., Dickinson, M., 2005, Corrected Least Squares method for aeroServoelasticity studies,Le 20e Congrès Canadien de Mécanique Appliquée à l’Université McGill, Montréal, Québec, Canada, 30 mai - 2 juin.

  190. Hiliuta, A., Botez, R.M., Brenner, M., 2005, Approximation of unsteady aerodynamic forces by use of fuzzy techniques, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Austin, Texas, États-Unis, 18-21 avril.

  191. Nadeau Beaulieu M., Popov A.-V., Popescu R., Hiliuta, A., Botez R. M., Mureithi, N., 2005, Methodology for Aerodynamic Model Generation for the B-427 Helicopter in Hover and Forward Flight by use of Flight Test Data, 11th Australian International Aerospace Congress, Melbourne, Australie, 13-17 mars.

  192. Crisan E. G., Botez R., Seto J., Lambert E., Hui K., Mureithi N.,2005,Applications of Parameter Estimation Methods in Helicopter Identification, 11th Australian International Aerospace Congress, Melbourne, Australie, 13-17 mars.

  193. Nadeau Beaulieu M., Hiliuta A., Popov A-V., Botez R.M., Mureithi, N., 2005, New Formulation of the Ground Dynamics Model Generation and Validation by use of Flight Test Data, 11th Australian International Aerospace Congress, Melbourne, Australie, 13-17 mars.

  194. Hiliuta, A., Botez, R.M., 2005, Approximation of unsteady aerodynamic forces by use of fuzzy theory, The IASTED Modeling, Identification and Control (MIC 2005) Conference, Innsbruck, Autriche, 14-18 février.

  195. Botez, R. M., Hiliuta, A., 2004, Aerodynamic forces formulation for aircraft aeroservoelasticity  studies, The AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence, Rhode Island, États-Unis, 16-19 août.

  196. Botez, R.M., Cotoi, I. and Dinu, A., 2004, Model order reduction for aeroservoelasticity studies by use of LRSRM and LRSM algorithms, ICAS Conference, Yokohama, Japon, 1-3 septembre.

  197. Botez, R.M., Ibrir, S., Biskri, D., Hamza, D., 2003, Aerodynamic forces approximation for aeroservoelastic models, The 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Paper AIAA-2003-7446, Norfolk, Virginie, États-Unis, 7-11 avril.

  198. Ibrir, S., Botez, R.M., 2003, Robust stabilization of uncertain aircraft models, The 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Paper AIAA-2003-7530, Norfolk, Virginie, États-Unis, 7-11 avril.

  199. Ibrir, S., Botez, R.M., 2003, A new approach to aeroservoelastic modelling, The 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Paper AIAA-2003-7537, Norfolk, Virginie, États-Unis, 7-11 avril.

  200. Botez, R.M., Biskri, D., Cotoi, I., Hamza, D., Herda, M., 2003, Unsteady aerodynamic forces methods for aeroservoelasticity studies, International Forum on Aeroelasticity and Structural Dynamics IFASD 2003, Amsterdam, Holland, 4-6 juin.

  201. Botez, R., Cotoi, I., Doin, A., Biskri, D., 2002, Method validation for aeroservoelastic analysis, The 43rd  AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, Paper AIAA 2002-1428, Denver, Colorado, États-Unis, 23-35 avril.

  202. Botez, R., Cotoi, I., 2002, Method for flutter aeroservoelastic open loop analysis, The 5th ASME Symposium on Fluid-Structure Interactions, Aeroelasticity, Flow Induced Vibrations and Noise, New Orleans, Louisiana, États-Unis, 17-22 novembre.

  203. Aouf, N., Boulet, B., Botez, R., 2002, A gain scheduling approach for a flexible  aircraft, The American Control Conference ACC, Article ACC02-AIAA1041, Alaska, États-Unis.

  204. Cotoi, R., Botez, R., 2002, Use of the MS Flight Simulator in the teaching of the   Introduction to avionics course, The ASEE Conference, Paper 2002-1928, Aerospace  Division, Montréal, Québec, Canada.

  205. Cotoi, I., Botez, R.M., 2001, Optimization of unsteady aerodynamic forces for aeroservoelastic analysis, The IASTED International Conference on Control and  Applications CA2001, Banff, Alberta, Canada, pp. 105-108, 27 - 29 juin.

  206. Bigras, P., Wong, T., Botez, R., 2001, Pressure tracking control of a double restriction pneumatic system, The IASTED International Conference on Control and Applications CA2001, Banff, Alberta, Canada, pp. 273-278, 27 - 29 juin.

  207. Botez, R.M., Parvu, P., Doin, A., 2001, Aeroservoelastic interactions on a flexible aircraft, The CANCAM Conference, St. John’s, Canada, pp. 187-188, 3 - 7 juin.

  208. Aouf, N., Boulet, B. et Botez, R. M., 2001, Model and controller reduction for flexible aircraft  preserving robust performance, The American Control Conference ACC,  Arlington, VA, États-Unis, Vol. 6, pp. 4758-4764, 25-27 juin.

  209. Aouf, N., Boulet, B. et Botez, R. M., 2000, H2 and Hinf  optimal gust load alleviation for a flexible  aircraft, The American Control Conference ACC, Chicago, États-Unis, Vol. 3, pp. 1872-1876, 7-9 juin.

  210. Aouf, N., Boulet, B. et Botez, R., 2000, Robust gust load alleviation for a flexible aircraft, The 47th Annual CASI Conference, Ottawa, Canada, pp. 95-104, 30 April - 3 mai.

  211. Bigras, P., Saad, M., O'Shea, J. et Botez, R., 2000, Inverse flexible manipulator model algorithm with convergence analysis, The 31st International Symposium on Robotics ISR 2000, Montréal, Québec, Canada, pp. 162-167, 14-17 juin.

  212. Botez, R.M., Bigras, P., 1999, Optimization of generalized aerodynamic forces for the aeroservoelasticity, The 3rd International Conference on Engineering Aero-Hydroelasticity,  Prague, Czech Republic, pp. 122-128, 30 août, 3 septembre.

  213. Botez, R.M., Boustani, I., Vayani, N., 1999, Active vibration control for a flexible aircraft equipped with gust load control system, The 6th International Congress on Sound and Vibration, Copenhagen, Denmark, pp. 1731-1738, 5 – 8 juillet.

  214. Botez, R.M., Bigras, P., 1999, Aerodynamic approximation of unsteady forces for the aeroservoelasticity study, The 46th CASI Canadian Aeronautics and Space Institute Annual Conference, Montréal, Québec, Canada, pp. 155-161, 2 – 5 mai. 

  215. Botez, R.M., Boustani, I., Vayani, N., 1999, Optimal control laws for gust alleviation, The 46th CASI Canadian Aeronautics and Space Institute Annual Conference, Montréal, Canada, pp. 649-655, 2 - 5 mai.





Notes de cours et de laboratoire a l'ÉTS
 
  1. GPA-745 Introduction à l’avionique

  2. GPA-741 Systèmes de commande des avions

  3. GPA-305 Élements de résistance des matériaux




 
Chapitres des livres écrits par invitation
 
  1. Grigorie, L.T., Botez, R. M., 2013, Modelling and simulation based Matlab/Simulink of a strap-down inertial navigation system’s errors due to the inertial sensors, Matlab book, INTECH Edition.

  2. Grigorie, L.T., Botez, R. M., Popov, A. V., 2012, Fuzzy logic control of a smart actuation system in a morphing wing, fuzzy controllers, ISBN: 979-953-307-843-3, INTECH Edition.

  3. Grigorie, L.T., Botez, R. M., 2011, Applications of fuzzy logic in the design and control of a morphing wing, using smart material actuators, fuzzy controllers, Theory and Applications, INTECH Edition.

  4. Grigorie, L.T., Botez, R. M., Popov, A. V., 2011, Morphing wing used shape memory alloy actuators new control technique with bi-Positional and PI laws optimum combination, Numerical and experimental validation, Lecture Notes in Electrical Engineering, Springer-Verlag.