Nhan Nguyen
Nhan Nguyen
NASA Ames Research Center
Email verificata su
Citata da
Citata da
Model-reference adaptive control
NT Nguyen, NT Nguyen
Model-Reference Adaptive Control: A Primer, 83-123, 2018
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
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
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
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
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
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
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
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
Drag optimization study of variable camber continuous trailing edge flap (VCCTEF) using OVERFLOW
UK Kaul, NT Nguyen
32nd AIAA applied aerodynamics conference, 2444, 2014
Optimal control modification for robust adaptive control with large adaptive gain
NT Nguyen
Systems & Control Letters 61 (4), 485-494, 2012
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
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
Elastically shaped future air vehicle concept
N Nguyen
NASA Innovation Fund Award, 2010
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
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
Flight dynamics of flexible aircraft with aeroelastic and inertial force interactions
N Nguyen, I Tuzcu
AIAA atmospheric flight mechanics conference, 6045, 2009
Blading system and method for controlling structural vibrations
N Nguyen
US Patent 6,102,664, 2000
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
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
Il sistema al momento non pu eseguire l'operazione. Riprova pi tardi.
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