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Stabilität
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keywords:(Stabilität)
A Robust Uniform Control Approach for VTOL Aircraft
A Robust Uniform Control Approach for VTOL Aircraft
Flow force regulation of the main poppet in a large flow load control valve
Synthesis of autonomous periodic motion of a small blimp system using the van der Pol equation
Transport system for sensitive goods based on electrorheological fluids
Airplane State Awareness Research Safety Enhancements
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
Advancing Electric Propulsion Aircraft Evaluation for Urban Air Mobility: Insights from NASA-Ames
Development of the Mod II X-57 Piloted Simulator and Flying Qualities Predictions
Entwicklung einer Vorderachsfederung für Spezialtraktoren
Aeroelastic Simulation of Transonic Truss-Braced Wing Aircraft for Flight Dynamic Stability Analysis
Aircraft Loss of Control: Research and Technology Summary & Future Directions
Aircraft Loss of Control: Research and Technology Summary & Future Directions
Mechatronische Antriebs- und Lenkkonzepte für Schienenfahrzeuge der nächsten Generation
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Control Concepts for Simplified Vehicle Operations of a Quadrotor eVTOL Vehicle
Mode-Based Sensing and Actuation Techniques for Multi-Objective Flexible Aircraft Control
Breakout: (Aircraft) Ride Quality and Passenger Experience
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
Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft
The posture control of a two-link free flying acrobot with initial angular momentum
Kinetic stability and propellant performance of Green energetic materials
Aircraft System Identification from Multisine Inputs and Frequency Responses
Free-flight and free-oscillation techniques for wind-tunnel dynamic-stability testing
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
Guidance, Navigation, and Control Analysis Activities at MSFC
Estimation, Navigation and Control of Multi-Rotor Drones in an Urban Wind Field
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
Common Rail Systeme zur Erreichung künftiger EU-Emissionsstandards
Real-Time Global Nonlinear Aerodynamic Modeling for Learn-To-Fly