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YOLOv4 Object Detection Model for Nondestructive Radiographic Testing in Aviation Maintenance Tasks
Worst-Case Disturbances for Time-Varying Systems with Application to Flexible Aircraft
Worst-Case Analysis of Complex Nonlinear Flight Control Designs Using Deep Q-Learning
Wind-Tunnel Study of the Autoregressive Moving-Average Flutter Prediction Method
What Was Learned in Predicting Slender Airframe Aerodynamics with the F-16XL Aircraft
Wake Turbulence Evolution and Hazard Analysis for General Aviation Takeoff Accident
Visualization of Nonlinear Aerodynamic Phenomena During F-16 Limit-Cycle Oscillations
Vision-Based Wind and Position Estimation with Fixed-Wing Unmanned Aerial Vehicle
Vibrational Energy Transfer and Collision-Induced Dissociation in Collisions
Vertical Wind-Tunnel Testing of Steerable Cruciform Parachute System
Vertically Optimal Close Formation Flight Control Based on Wingtip Vortex Structure
Verifying the Effect of Wingtip Propellers on Drag Through In-Flight Measurements
Vent Valve for Test Launch Vehicle of Korea Space Launch Vehicle II
Venting Analysis of the Payload Fairing of Korea Space Launch Vehicle II
Validation of Numerical Virtual Flight System with Wind-Tunnel Virtual Flight Testing
Using -Limited , Controllability Issues on Contaminated Runways and in Crosswind
Use of Time-Frequency Representations for Interpreting Handling Qualities Flight Test Data
Unsteady Three-Dimensional Mode Transition Phenomena in a Scramjet Flowpath
Unsteady Surface Pressure Characterization on Launch Vehicle in Liftoff Configuration
Unsteady Aerodynamic Modeling of Aircraft Control Surfaces by Indicial Response Methods
Unsteady Aerodynamic Loads on a High-Agility Aircraft due to Wake Vortex Encounter
Unstart Process of a Rectangular Hypersonic Inlet at Different Mach Numbers
Unified Velocity Control and Flight State Transition of Unmanned Tilt-Wing Aircraft
Unified Framework for Training Point Selection and Error Estimation for Surrogate Models
Underwing Missile Control-Surface Effects on Aircraft Limit Cycle Oscillations
Underwing Missile Aerodynamic Effects on Flight-Measured Limit-Cycle Oscillations
Uncertainty Reduction in Aeroelastic Systems with Time-Domain Reduced-Order Models
Ultra-Wideband Localization and Deep-Learning-Based Plant Monitoring Using Micro Air Vehicles
Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints for Unsteady Flow Measurement
UH-60A Rotor Structural Loads Analysis with Fixed System Structural Dynamics Modeling
Two-Stage Batch Algorithm for Nonlinear Static Parameter Estimation
Turbulent Airwake Estimation from Helicopter–Ship Wind-Tunnel Data
Trim Calculation of the CH-53 Helicopter Using Numerical Continuation Method
Trigger Mechanism for Obtaining Dynamic Derivatives in Wind Tunnels Using Free-Oscillation Technique
Transitional Flight of Tail-Sitter Unmanned Aerial Vehicle Based on Multiple-Model Adaptive Control
Transitional Control Architecture and Methodology for a Twin Rotor Tailsitter
Transient Plasma Wind Tunnel Testing Under Thermomechanical Loads for Reentry Break-Up Analysis
Transforming Civil Helicopters into Personal Aerial Vehicles: Modeling, Control, and Validation
Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation
Toward Objective Assessment of Simulation Predictive Capability
Time-Varying Model Identification of Flapping-Wing Vehicle Dynamics Using Flight Data
Three-Temperature Thermochemical Nonequilibrium Model with Application to Slender-Body Wakes