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Standsicherheit
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A numerical study on constant spacing policies for starting platoons at oversaturated intersections
A Robust Uniform Control Approach for VTOL Aircraft
NASA Armstrong Flight Research Center Dynamics and Controls (530)
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Multipropeller Whirl Flutter Stability Study using Component Mode Synthesis Element
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions
Aircraft Loss of Control: Research and Technology Summary & Future Directions
Aircraft Loss of Control: Research and Technology Summary & Future Directions
Advancing Electric Propulsion Aircraft Evaluation for Urban Air Mobility: Insights from NASA-Ames
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Multipropeller Whirl Flutter Stability Study using Component Mode Synthesis Element
An L1 Adaptive Control Augmentation for a Lift + Cruise Vehicle
Understanding a Kepler 2-Wheel Mission
Airplane State Awareness Research Safety Enhancements
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Modeling of Large-Amplitude High-Angle-of-Attack Maneuvers
Breakout: (Aircraft) Ride Quality and Passenger Experience
CPAS Main Parachute Cluster Asymmetry: A Second Look
NASA Armstrong Flight Research Center Dynamics and Controls (530)
Guidance, Navigation, and Control Analysis Activities at MSFC
Laminar to Turbulence Transition in Boundary Layers Due to Tripping Devices
Further Evaluation of the Efficacy of SEL Related to Annoyance to Helicopter Maneuvers
Challenges and Opportunities in Autonomous Flight
The Impact of Structural Vibration on Flying Qualities of a High Speed Civil Transport
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft
Multi-Vehicle Cooperative Control Research NASA Dryden Flight Research Center 1998 - 2012
Cartesian Mesh Simulations and Farfield Propagation Results
Airplane stability calculations and their verification by flight tests
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft
Peak-Seeking Optimization of Spanwise Lift Distribution for Wings in Formation Flight
Lessons from Modeling Flexible Aircraft for Active Flutter Suppression
Engine Yaw Augmentation for Hybrid-Wing-Body Aircraft via Optimal Control Allocation Techniques
Quadrocopter Control Design and Flight Operation
Flight Test Approach to Adaptive Control Research
NASA Dryden Flight Research Center's Space Weather Needs
Advances in Aircraft System Identification at NASA Langley Research Center