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Stabilität
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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
New Flutter Analysis Technique for Time-Domain Computational Aeroelasticity
Variable Geometry Aircraft Wing Supported by Struts And/Or Trusses