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Flugmechanik
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Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Linear, Parameter Varying Model Reduction for Aeroservoelastic Systems
An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft
Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism
Using Indirect Turbulence Measurements for Real-Time Parameter Estimation in Turbulent Air
LQR Controller for Stabilization of Flapping Wing MAV in Gust Environments
Ground Vibration Test Identified Structure Model for Flutter Envelope Prediction
Parafoil Control Using Payload Weight Shift
Robust Parafoil Terminal Guidance Using Massively Parallel Processing