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Flugmechanik
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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
Parametric Study of Powered Parafoil Flight Dynamics
Nonlinear Unsteady Aerodynamic Modeling by Volterra Variational Approach
Parameter Estimation of Highly Unstable Aircraft Assuming Linear Errors
Parametric Modeling for Store Separation Aerodynamics Using System Identification
Simulation of Flight Dynamics with an Improved Post-Stall Aerodynamics Model
Design, Simulation, and Experimental Testing of Humanitarian Aid Airdrop Micro Packages
Eigenvalue Constraints for Realization-Based Identification
Investigation of Trajectory Generation for a Mission Adaptive Planetary Entry Guidance Algorithm
Safe Set Maneuverability of Impaired Aircraft
Low-Order Modeling For A Small-Scale Flybarless Helicopter UAV A Grey-Box Time-Domain Approach
Aeroelastic Effects of Battens on the Flight Dynamics of a MAV
Model Predictive Control of Agile Projectiles
Subcritical Bifurcations in Shimmy Dynamics
Flight Control Development for a Speed-Agile Powered-Lift Transport Aircraft
Ground Contact Model for Mars Science Laboratory Mission Simulations
Feasibility Study of a Novel Method for Real-Time Aerodynamic Coefficient Estimation
Nonlinear Model Reduction for Flexible Aircraft Control Design
Aerodynamic Effects of Parafoil Upper Surface Bleed Air Actuation
Design Evolution of a High Packing Density Micro Air Vehicle for Local-Area Seeding
Computational 3D Icing Results for Scaled DLR-F6 Geometry
Aircraft Dynamic Modeling in Turbulence
Bifurcation Analysis of the NASA GTM with a View to Upset Recovery
Model-based Aerodynamic-angle Attitude Control of an Atmospheric Entry Capsule
Survey of Blunt Body Dynamic Stability in Supersonic Flow
Center of Gravity Estimation of an Aircraft Solely Using Standard Aircraft Measurement Sensors
Application of Sweet Spot Determination to a Conventional Pair of Aircraft
Airship Waypoint Navigation in the Presence of Wind
Trajectory Optimization Studies of Long Range Morphing Projectiles
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