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Nhan T. Nguyen
Researcher at Ames Research Center
Publications - 201
Citations - 3414
Nhan T. Nguyen is an academic researcher from Ames Research Center. The author has contributed to research in topics: Adaptive control & Aeroelasticity. The author has an hindex of 28, co-authored 201 publications receiving 2837 citations. Previous affiliations of Nhan T. Nguyen include Scripps Research Institute.
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Journal ArticleDOI
Antitumor activity of a systemic STING-activating non-nucleotide cGAMP mimetic
Emily N. Chin,Chenguang Yu,Chenguang Yu,Vincent F. Vartabedian,Ying Jia,Manoj Kumar,Ana M. Gamo,William Vernier,Sabrina H. Ali,Mildred Kissai,Daniel C. Lazar,Nhan T. Nguyen,Laura E. Pereira,Brent Benish,Ashley K. Woods,Sean B. Joseph,Alan Chu,Kristen Johnson,Philipp N. Sander,Francisco Martínez-Peña,Eric Hampton,Travis S. Young,Dennis W. Wolan,Arnab K. Chatterjee,Peter G. Schultz,Peter G. Schultz,H. Michael Petrassi,John R. Teijaro,Luke L. Lairson +28 more
TL;DR: A non-nucleotide, small-molecule STING agonist, termed SR-717, that demonstrates broad interspecies and interallelic specificity and functions as a direct cyclic guanosine monophosphate–adenosine monophile mimetic that induces the same “closed” conformation of STING.
Journal ArticleDOI
Flight Dynamics and Hybrid Adaptive Control of Damaged Aircraft
TL;DR: In this paper, a neural network hybrid direct-indirect adaptive flight control is developed for the stability augmentation control of the damaged aircraft. But, this approach is limited to a single aircraft.
Proceedings ArticleDOI
Dynamics and Adaptive Control for Stability Recovery of Damaged Asymmetric Aircraft
TL;DR: A preliminary simulation of the hybrid adaptive flight control has been performed and initial data have shown the effectiveness of the proposed hybrid approach, which is an adaptive law derived from the Lyapunov stability theory for stabilizing the rotational motion of the damaged aircraft.
Proceedings ArticleDOI
A Mission-Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift-to-Drag Ratios of Future N+3 Transport Aircraft
TL;DR: The VCCTEF program is developing better lift and drag performance of flexible wing transports with the further benefits of lighter-weight actuation and less drag using the variable camber shape of the flap.
Proceedings ArticleDOI
An Optimal Control Modification to Model-Reference Adaptive Control for Fast Adaptation
TL;DR: In this paper, a method that can achieve fast adaptation for a class of model-reference adaptive control is presented, based on the minimization of the squares of the tracking error, which is formulated as an optimal control problem.