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Flugmechanik
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Investigation of Optimal Control Allocation for Gust Load Alleviation in Flight Control
Prediction of Aircraft Spin Characteristics by Continuation and Bifurcation Methods
A Multi-Model Gauss Pseudospectral Optimization Method for Aircraft Trajectories
Forced Oscillation Wind Tunnel Testing for FASER Flight Research Aircraft
Optimization of Engine Failure on a Flying Wing Configuration
Aerodynamic Sensing for a Fixed Wing UAS Operating at High Angles of Attack
Unmanned Aircraft and the Applicability of Military Flying Qualities Standards
Aeroelastic Effects of Wing Stiffness on the Flight Dynamics of a MAV
Effects of Freeplay on Aircraft Main Landing Gear Stability
Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel Data
Investigation of the Prediction Error Identification for Flutter Prediction
Aerodynamic Model Identification of Frauke UAV
Development of a Fundamental Model for Flapping Wing MAVs and Preliminary Validation
Performance Enhancements by Bounding Flight
System Identification of Flexible Aircraft in Time Domain
Aircraft Spin Phenomenon Analysis Using Nonlinearity Index Theory
Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Linear, Parameter Varying Model Reduction for Aeroservoelastic Systems