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Stabilität
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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
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
An L1 Adaptive Control Augmentation for a Lift Plus-Cruise Vehicle
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Control Concepts for Simplified Vehicle Operations of a Quadrotor eVTOL Vehicle
Airplane State Awareness Research Safety Enhancements
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions
Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction
Modeling of Large-Amplitude High-Angle-of-Attack Maneuvers
Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
Mode-Based Sensing and Actuation Techniques for Multi-Objective Flexible Aircraft Control
Breakout: (Aircraft) Ride Quality and Passenger Experience
Free-flight and free-oscillation techniques for wind-tunnel dynamic-stability testing
Aircraft System Identification from Multisine Inputs and Frequency Responses
Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft
NASA Armstrong Flight Research Center Dynamics and Controls (530)
Piloted Simulator Evaluation Results of Flight Physics Based Stall Recovery Guidance
Learn-To-Fly (L2F): Real-Time Modeling, Learning Control, and Guidance for Autonomous Flight
Simulation Evaluation of Pilot Inputs for Real Time Modeling During Commercial Flight Operations
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
Aeroelastic Modeling of X-56A Stiff-Wing Configuration Flight Test Data
Real-Time Global Nonlinear Aerodynamic Modeling for Learn-To-Fly
Estimation, Navigation and Control of Multi-Rotor Drones in an Urban Wind Field
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
Toward n-Ship Computation of Trajectories for Shared Airspace
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Establishing a Disruptive New Capability for NASA to Fly UAV's into Hazardous Conditions
Design and Analysis of Morpheus Lander Flight Control System