| Flight dynamics and hybrid adaptive control of damaged aircraft N Nguyen, K Krishnakumar, J Kaneshige, P Nespeca Journal of guidance, control, and dynamics 31 (3), 751-764, 2008 | 166 | 2008 |
| Model-reference adaptive control NT Nguyen, NT Nguyen Model-Reference Adaptive Control: A Primer, 83-123, 2018 | 161 | 2018 |
| Dynamics and adaptive control for stability recovery of damaged asymmetric aircraft N Nguyen, K Krishnakumar, J Kaneshige, P Nespeca AIAA Guidance, navigation, and control Conference and Exhibit, 6049, 2006 | 124 | 2006 |
| An optimal control modification to model-reference adaptive control for fast adaptation N Nguyen, K Krishnakumar, J Boskovic AIAA Guidance, Navigation and Control Conference and Exhibit, 7283, 2008 | 113 | 2008 |
| Multiple-model adaptive fault-tolerant control of a planetary lander JD Boskovic, JA Jackson, RK Mehra, NT Nguyen Journal of Guidance, Control, and Dynamics 32 (6), 1812-1826, 2009 | 108 | 2009 |
| A mission adaptive variable camber flap control system to optimize high lift and cruise lift to drag ratios of future N+ 3 transport aircraft J Urnes, N Nguyen 51st AIAA aerospace sciences meeting including the new horizons forum and …, 2013 | 90 | 2013 |
| Design of neural network-based estimator for tool wear modeling in hard turning X Wang, W Wang, Y Huang, N Nguyen, K Krishnakumar Journal of intelligent manufacturing 19, 383-396, 2008 | 89 | 2008 |
| A set-theoretic model reference adaptive control architecture for disturbance rejection and uncertainty suppression with strict performance guarantees E Arabi, BC Gruenwald, T Yucelen, NT Nguyen International Journal of Control 91 (5), 1195-1208, 2018 | 73 | 2018 |
| Aeroelastic modeling of elastically shaped aircraft concept via wing shaping control for drag reduction N Nguyen, J Urnes AIAA Atmospheric Flight Mechanics Conference, 4642, 2012 | 68 | 2012 |
| Drag optimization study of variable camber continuous trailing edge flap (VCCTEF) using OVERFLOW UK Kaul, NT Nguyen 32nd AIAA applied aerodynamics conference, 2444, 2014 | 61 | 2014 |
| Optimal control modification for robust adaptive control with large adaptive gain NT Nguyen Systems & Control Letters 61 (4), 485-494, 2012 | 58 | 2012 |
| Elastically shaped future air vehicle concept N Nguyen NASA Innovation Fund Award, 2010 | 53 | 2010 |
| Development of variable camber continuous trailing edge flap for performance adaptive aeroelastic wing N Nguyen, U Kaul, S Lebofsky, E Ting, D Chaparro, J Urnes SAE AeroTech Congress & Exhibition, 2015 | 50 | 2015 |
| Elastically shaped wing optimization and aircraft concept for improved cruise efficiency N Nguyen, K Trinh, K Reynolds, J Kless, M Aftosmis, J Urnes 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2013 | 43 | 2013 |
| Blading system and method for controlling structural vibrations N Nguyen US Patent 6,102,664, 2000 | 42 | 2000 |
| Flight dynamics of flexible aircraft with aeroelastic and inertial force interactions N Nguyen, I Tuzcu AIAA atmospheric flight mechanics conference, 6045, 2009 | 37 | 2009 |
| Optimization of variable-camber continuous trailing-edge flap configuration for drag reduction E Ting, D Chaparro, N Nguyen, GEC Fujiwara Journal of Aircraft 55 (6), 2217-2239, 2018 | 36 | 2018 |
| Stability limit of human-in-the-loop model reference adaptive control architectures T Yucelen, Y Yildiz, R Sipahi, E Yousefi, N Nguyen International Journal of Control 91 (10), 2314-2331, 2018 | 34 | 2018 |
| LPV modeling of a flexible wing aircraft using modal alignment and adaptive gridding methods AK Al-Jiboory, G Zhu, SSM Swei, W Su, NT Nguyen Aerospace science and technology 66, 92-102, 2017 | 33 | 2017 |
| Experimental investigation of a flexible wing with a variable camber continuous trailing edge flap design NT Nguyen, E Livne, N Precup, JM Urnes, C Nelson, E Ting, S Lebofsky 32nd AIAA Applied Aerodynamics Conference, 2441, 2014 | 33 | 2014 |
