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A Robust Uniform Control Approach for VTOL Aircraft
A Robust Uniform Control Approach for VTOL Aircraft
Multipropeller Whirl Flutter Stability Study using Component Mode Synthesis Element
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Understanding a Kepler 2-Wheel Mission
Reference Command Optimization for the Transition Flight Mode of a Lift plus Cruise Vehicle
NASA Armstrong Flight Research Center Dynamics and Controls (530)
System Identification of Flexible Aircraft: Lessons Learned from the X-56A Phase 1 Flight Tests
Control of Flexible Spacecraft with Structural Feedback
Free-Flight CFD Simulations and Dynamic StabilityAnalysis of the Orion Crew Module
Preliminary Steps in Developing Rapid Aero Modeling Technology
Airplane State Awareness Research Safety Enhancements
Advancing Electric Propulsion Aircraft Evaluation for Urban Air Mobility: Insights from NASA-Ames
Dynamic Aeroelastic Flight Dynamic Modeling of Mach 0.745 Transonic Truss-Braced Wing
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Modeling of Large-Amplitude High-Angle-of-Attack Maneuvers
The Impact of Structural Vibration on Flying Qualities of a Supersonic Transport