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James Urnes

Observed names: J. URNES, J. Urnes, J.M. Urnes, JAMES URNES, James M. Urnes, James M. Urnes, Sr., James Urnes Sr, Urnes, James M.
OpenAlex ID: A5085959876
A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft
2013 · James Urnes, Nhan Nguyen · AIAA Aerospace Sciences Meeting · 148
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Aeroelastic Modeling of Elastically Shaped Aircraft Concept via Wing Shaping Control for Drag Reduction
2012 · Nhan Nguyen, James Urnes · AIAA Atmospheric Flight Mechanics Conference · 120
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Development of the F/A-18A automatic carrier landing system
1985 · J.M. Urnes, R.K. Hess · Journal of Guidance Control and Dynamics · 113
Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency
2013 · Nhan Nguyen, Khanh Trinh, et al. · AIAA Aerospace Sciences Meeting · 91
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Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design
2014 · Nhan T. Nguyen, Eli Livne, et al. · AIAA Applied Aerodynamics Conference · 71
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Development of Variable Camber Continuous Trailing Edge Flap for Performance Adaptive Aeroelastic Wing
2015 · Nhan Nguyen, Sonia Lebofsky, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 64
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Wind Tunnel Investigation of a Flexible Wing High-Lift Configuration with a Variable Camber Continuous Trailing Edge Flap Design
2015 · Nhan T. Nguyen, Nathan Precup, et al. · AIAA Applied Aerodynamics Conference · 37
Flight demonstration of the self-repairing flight control system in a NASA F-15 aircraft
1991 · JAMES URNES, ROBERT YEAGER · Aircraft Design and Operations Meeting · 28
Dynamic Flight Envelope Assessment and Prediction
2008 · James Urnes, Eric Reichenbach, et al. · AIAA Guidance, Navigation, and Control Conference and Exhibit · 27
Fast On-Line Actuator Reconfiguration Enabling (FLARE) System
2005 · Jovan Boskovic, Sarah Bergstrom, et al. · AIAA Guidance, Navigation, and Control Conference and Exhibit · 22
Use of Propulsion Commands to Control Directional Stability of a Damaged Transport Aircraft
2010 · James Urnes, Zach Nielsen · AIAA Infotech@Aerospace Conference · 13
Development of the Navy H-Dot Automatic Carrier Landing System designed to give improved approach control in air turbulence
1979 · J. URNES, R. HESS, et al. · Guidance and Control Conference · 12
A damage adaptive flight control system using neural network technology
2001 · J. Urnes, R. Davidson, et al. · Proceedings of the ... American Control Conference/Proceedings of the American Control Conference · 10
Control System Design for a Variable Camber Continuous Trailing Edge Flap System on an Elastic Wing
2014 · Charles Morris, James Sheahan, et al. · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 9
Adaptive reconfigurable control based on a reduced order system identification for flutter and aeroservoelastic instability suppression
2001 · C. Nam, P. Chen, et al. · AIAA Applied Aerodynamics Conference · 8
Using neural networks for aerodynamic parameter modeling
2005 · G. Peterson, W. Bond, et al. · Proceedings of the ... American Control Conference/Proceedings of the American Control Conference · 7
Reconfigurable control and fault identification system
2005 · S. Black, K. Keller, et al. · IEEE Aerospace Conference (AERO) · 7
Design and Flight Test of an Intelligent Flight Control System
2010 · Tim Smith, Jim Barhorst, et al. · Studies in computational intelligence · 6
Dynamic Structural Fault Detection and Identification
2009 · Timothy Smith, Zach Nielsen, et al. · AIAA Guidance, Navigation, and Control Conference and Exhibit · 6
Wing shaping concepts using distributed propulsion
2014 · Kevin Reynolds, Nhan Nguyen, et al. · Aircraft Engineering and Aerospace Technology · 5
Active Control for Elastic Wing Structure Dynamic Modes
2015 · James M. Urnes, John R. Dykman, et al. · AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (SDM) · 4
Flight Control for Multi-Engine UAV Aircraft Using Propulsion Control
2012 · James Urnes · AIAA Infotech@Aerospace Conference · 4
Performance Evaluation of an Integrated Retrofit Failure Detection, Identification and Reconfiguration (FDIR) System Using High-Fidelity and Piloted Simulations
2004 · Jovan D. Bošković, Sarah E. Bergstrom, et al. · SAE technical papers on CD-ROM/SAE technical paper series · 3
Adaptive Reconfigurable Control Based on a Reduced Order System Identification for Flutter and Aeroservoelastic Instability Suppression
2000 · C. Nam, P. C. Chen, et al. · Defense Technical Information Center (DTIC) · 3
Use of Propulsion Commands to Prevent Loss-of-Control Aircraft Accidents
2011 · James Urnes, Timothy Smith · AIAA Infotech@Aerospace Conference · 2
Works count: 39
Citation count: 824
H-index: 12
I10-index: 13
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