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Stabilität
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keywords:(Stabilität)
Initial Assessment of Stability and Controllability in the Early Stage of Combat Aircraft Design
Breakout: (Aircraft) Ride Quality and Passenger Experience
NASA Armstrong Flight Research Center Dynamics and Controls (530)
Lessons from Modeling Flexible Aircraft for Active Flutter Suppression
Stability and Control Derivative Estimation for the Bell-Shaped Lift Distribution
Verification and Validation Challenges for Adaptive Flight Control of Complex Autonomous Systems
Guidance, Navigation, and Control Analysis Activities at MSFC
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression
Optimal Control Allocation with Load Sensor Feedback for Active Load Suppression
Active Dihedral Control System for a Torsionally Flexible Wing
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Dynamics and Control Work at NASA Armstrong
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
Variable Geometry Aircraft Wing Supported by Struts And/Or Trusses
Active Structural Control for Aircraft Efficiency with the X-56A Aircraft
Active Dihedral Control System for a Torisionally Flexible Wing
Flight Research: X-31A Enhanced Fighter Maneuverability and F-18 High Alpha Research Vehicle
Where to Land: A Reachability Based Forced Landing Algorithm for Aircraft Engine Out Scenarios
NASA Armstrong Flight Research Center Dynamics and Controls Branch
Airborne Simulation of Launch Vehicle Dynamics
Aeroelastic Tailoring Study of N+2 Low-Boom Supersonic Commercial Transport Aircraft
Approach for Structurally Clearing an Adaptive Compliant Trailing Edge Flap for Flight
Artificial Immune System Approach for Airborne Vehicle Maneuvering
Variable Geometry Aircraft Pylon Structure and Related Operation Techniques
Pain Compensating Control for Structural Overload Prevention
Piloted Simulation of a Model-Predictive Automated Recovery System
Application and Evaluation of Control Modes for Risk-Based Engine Performance Enhancements
Structural Pain Compensating Flight Control
Multi-Vehicle Cooperative Control Research at the NASA Armstrong Flight Research Center, 2000-2014
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft
Entry, Descent and Landing Systems Short Course
Reverse Engineering Crosswind Limits - A New Flight Test Technique?
Multi-Vehicle Cooperative Control Research NASA Dryden Flight Research Center 1998 - 2012
Beyond Rigid Body: Integrated Structural Control of Extremely Lightweight Flexible Aircraft
Peak-Seeking Optimization of Spanwise Lift Distribution for Wings in Formation Flight
Quadrocopter Control Design and Flight Operation