FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER
DEMONSTRATION OF PROP-ROTOR SYSTEM DEVELOPMENT FOR 52KG MTOW QUAD-TILT PROP UAV
DEMONSTRATION OF PROP-ROTOR SYSTEM DEVELOPMENT FOR 52KG MTOW QUAD-TILT PROP UAV
A side-chain crosslinking approach for the fabrication of conjugated polymer patterns
Numerical Study of Effect of Control Surface on Wing Flutter in Transonic Flow (AIAA 2014-1200)
HSG Control Strategy improving Fuel Economy and NVH Performance for TMED HEV
Rollover Initiation Simulations for Designing Rollover Initiation Test System (RITS)
The Nuclear Cryogenic Propulsion Stage (AIAA 2014-4171)
Aerodynamic Design of EAV Propeller using a Multi-Level Optimization Method
A Nuclear Cryogenic Propulsion Stage for Near-Term Space Missions
Flexible VOC sensors using conductive polymers and porous membranes for application to textiles
New reduced order modeling technique using aeroelastic time response data
Parametric Studies of Composite Blade to Improve the Wind Turbine Response
Transonic Flutter Analysis Using Coupled CFD-CSD Analysis and New Reduced Order Modeling Technique
Development of the Implementation Human Response Process for Objective Drivability Evaluation
Online State-of-Health Prediction of Lithium-Ion Battery with a Multiscale Filtering Technique
The Effects of Jatropha-derived Biodiesel on Diesel Engine Combustion and Emission Characteristics
AFFORDABLE DEVELOPMENT OF A NUCLEAR CRYOGENIC PROPULSION STAGE
Optimization of the Wind Turbine Rotor to Enhance the Performance
Follower-Force Experiments with Geometric Nonlinear Coupling for Analytical Validation
Design of power split transmission: Design of dual mode power split transmission
Design of power split transmission: Design of dual mode power split transmission
Design of power split transmission: Design of dual mode power split transmission
2010-9386 Separation Standards under Automated Separation Assurance
Experimental Determination of Unsteady Aerodynamic Coefficients for a Three Dimensional Rigid Wing