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Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
A Guide to Forced Oscillation Data Processing and Analysis
Stratospheric Test Methodology for Characterizing Free-Flight Dynamics of Entry Vehicles
Reconstruction of the Apollo 11 Moon Landing Final Descent Trajectory
Rapid Flight Control Law Deployment and Testing Framework for Subscale VTOL Aircraft
A Learn-to-Fly Approach for Adaptively Tuning Flight Control Systems
Investigation of High Incidence Angle Propeller Aerodynamics for Subscale eVTOL Aircraft
Air Traffic Management Technology Demostration-1 (ATD-1) Avionics Phase 2 Flight Test and Results
Simulation Evaluation of Pilot Inputs for Real Time Modeling During Commercial Flight Operations
Position Corrections for Airspeed and Flow Angle Measurements on Fixed-Wing Aircraft
Design and Control of an Experimental Tilt-Wing Aircraft
Vertical Motion Simulator Experiment on Stall Recovery Guidance
UAS Well Clear Recovery Against Non-Cooperative Intruders Using Vertical Maneuvers
Aerodynamic Design of the Hybrid Wing Body Propulsion-Airframe Integration
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
GOES-R Active Vibration Damping Controller Design, Implementation, and On-Orbit Performance
Development of Mission Adaptive Digital Composite Aerostructure Technologies (MADCAT)
ADEPT Sounding Rocket One (SR-1)Flight Experiment Overview
Integrated Insulation System for Automotive Cryogenic Storage Tanks
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
Capsulation Satellite or CapSat: A Low-Cost, Reliable, Rapid-Response Spacecraft Platform
Evaluating the Autonomous Flying Qualities of a Simulated Variable Stability Aircraft
Aerodynamic Design of Integrated Propulsion-Airframe Configuration of the Hybrid Wing-Body Aircraft
Design Requirements for Unmanned Rotorcraft Used in Low-Risk Concepts of Operation
Status of Computational Aerodynamic Modeling Tools for Aircraft Loss-of-Control
Investigation of Desiccants and CO2 Sorbents for Advanced Exploration Systems 2015-2016
Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA's Space Launch System
Nonlinear Unsteady Aerodynamic Modeling Using Wind Tunnel and Computational Data
Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Full-Scale Prop-Rotor Stability Tests on the XV3 at High Advance Ratios
Novel Control Effectors for Truss Braced Wing
Application and Evaluation of Control Modes for Risk-Based Engine Performance Enhancements
Use of Higher Fidelity Slosh Models to Reduce Conservatism in Launch Vehicle Flight Control Designs
Earth Entry Vehicle Design for Sample Return Missions Using M-SAPE
Application and Evaluation of Control Modes for Risk-Based Engine Performance Enhancements