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Absolute Navigation Performance of the Orion Exploration Flight Test 1
Acceleration Effects on the Cooling Performance of a Partially Confined FC-72 Spray
Accounting for Finite Flash Duration in Diffusivity Experiments
A Concept for Credibility Assessment of Aircraft System Simulators
Active Control of Aeroelastic Vibrations for Electromechanical Missile Fin Actuation Systems
Active Flow Control Computations: From a Single Actuator to a Complete Airplane
Adaptive Algorithm for Classifying Launch and Recovery of the HH-60H Seahawk
Adaptive Attitude Tracking with Active Uncertainty Rejection
Adaptive Three-Step Kalman Filter for Air Data Sensor Fault Detection and Diagnosis
Additive Manufacturing of Lightweight, Optimized, Metallic Components Suitable for Space Flight
Adjustable Frequency Fluidic Oscillator with Supermode Frequency
Advancements in the Theory and Practice of Flight Vehicle System Identification
Advances and Modern Applications of Frequency-Domain Aircraft and Rotorcraft System Identification
Advances in Aircraft System Identification at NASA Langley Research Center
Advances in Wall Interference Corrections for Two-Dimensional Lifting Bodies
Advancing Mistuning Identification and Dynamic Modeling of Blisks Through Blade Detuning Tests
Adversarial Learning Improves Vision-Based Perception from Drones with Imbalanced Datasets
Aerodynamic Coefficient Identification of a Space Vehicle from Multiple Free-Flight Tests
Aerodynamic Force Modeling of Multirotor Unmanned Aerial Vehicles
Aerodynamic Parameter Estimation for a Morphing Unmanned Aerial Vehicle from Flight Tests
Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements
Aerodynamic Parameter Identification and Uncertainty Quantification for Small Unmanned Aircraft
Aerodynamics Modeling and Analysis of Close Formation Flight
Aeroelastic Energy Analysis Using Distributed Aerodynamic Work Visualization
Aeroelastic Model for Macrofiber Composite Actuators on Micro Air Vehicles
Aeroelastic Semiphysical Simulation and Wind-Tunnel Testing Validation of a Fin–Actuator System
Aeroelastic System Identification for Flutter Prediction via Multi-Output Autoregressive Modeling
Aeromechanics of a Coaxial Ultralight Rotorcraft During Turn, Climb, and Descent Flight
Aeromechanics of Rigid Coaxial Rotor Models for Wind-Tunnel Testing
Aerostructural Performance of Distributed Compliance Morphing Wings: Wind Tunnel and Flight Testing
Aerothermal Prediction of Multiple Hot Jets in Crossflow for Aircraft Applications
Aerothermal–Structural Analysis of a Rocket-Launched Mach 8 Scramjet Experiment: Descent
Aircraft Inertial Measurement Unit Fault Identification with Application to Real Flight Data
Aircraft Loss of Control Problem Analysis and Research Toward a Holistic Solution
Aircraft System Identification from Multisine Inputs and Frequency Responses
Analysis of Effect of Ground Experiment Environment on Plasma Contactor Performance
Analysis of Residual Stresses Induced by Riveting Process and Fatigue Life Prediction
Analysis of Simulated Imagery for Real-Time Vision-Based Automated Aerial Refueling
Analysis of the X-15 Flight 3-65-97 Divergent Limit-Cycle Oscillation
Analytical and Experimental Power Minimization for Fixed-Pitch Coaxial Rotors in Hover