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Stabilität
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A Robust Uniform Control Approach for VTOL Aircraft
Airplane State Awareness Research Safety Enhancements
NASA Armstrong Flight Research Center Dynamics and Controls (530)
Aircraft Loss of Control: Research and Technology Summary & Future Directions
Aircraft Loss of Control: Research and Technology Summary & Future Directions
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions
Modeling of Large-Amplitude High-Angle-of-Attack Maneuvers
Advancing Electric Propulsion Aircraft Evaluation for Urban Air Mobility: Insights from NASA-Ames
Breakout: (Aircraft) Ride Quality and Passenger Experience
NASA Armstrong Flight Research Center Dynamics and Controls (530)
Guidance, Navigation, and Control Analysis Activities at MSFC
Further Evaluation of the Efficacy of SEL Related to Annoyance to Helicopter Maneuvers
Challenges and Opportunities in Autonomous Flight
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft
Airplane stability calculations and their verification by flight tests
NASA Dryden Flight Research Center's Space Weather Needs
Peak-Seeking Optimization of Spanwise Lift Distribution for Wings in Formation Flight
Multi-Vehicle Cooperative Control Research NASA Dryden Flight Research Center 1998 - 2012
Cartesian Mesh Simulations and Farfield Propagation Results
Lessons from Modeling Flexible Aircraft for Active Flutter Suppression
Flight Test Approach to Adaptive Control Research
Engine Yaw Augmentation for Hybrid-Wing-Body Aircraft via Optimal Control Allocation Techniques
Quadrocopter Control Design and Flight Operation
Advances in Aircraft System Identification at NASA Langley Research Center
Candidate Performance Metrics for Generalized Control for Autonomous Flight
Flight Test of L1 Adaptive Controller on the NASA AirSTAR Flight Test Vehicle
F-15 Intelligent Flight Control System and Aeronautics Research at NASA Dryden
L(sub 1) Adaptive Control Design for NASA AirSTAR Flight Test Vehicle
AERONAUTICAL LAB. EXAMINATION OF RECENT LATERAL-STABILITY-DERIVATIVE DATA
Implementation of an Adaptive Controller System from Concept to Flight Test
Pilot Evaluation of Adaptive Control in Motion-Based Flight Simulator
Variable-Structure Control of a Model Glider Airplane
Simulation Based Evaluation of Integrated Adaptive Control and Flight Planning Technologies