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A Robust Uniform Control Approach for VTOL Aircraft
A Robust Uniform Control Approach for VTOL Aircraft
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
Airplane State Awareness Research Safety Enhancements
Free-Flight CFD Simulations and Dynamic StabilityAnalysis of the Orion Crew Module
Preliminary Steps in Developing Rapid Aero Modeling Technology
Understanding a Kepler 2-Wheel Mission
An L1 Adaptive Control Augmentation for a Lift + Cruise Vehicle
Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
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
Dynamic Aeroelastic Flight Dynamic Modeling of Mach 0.745 Transonic Truss-Braced Wing
Multipropeller Whirl Flutter Stability Study using Component Mode Synthesis Element
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions