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Flugmechanik
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keywords:("Flugmechanik")
Physik des Fliegens, Strömungsphysik, Raketen, Satelliten
End-To-End Simulation of Launch Vehicle Trajectories Including Stage Separation Dynamics
Adaptive Control of Flow over Wind Turbine Blades
Bifurcation Analysis and Simulation of Stall and Spin Recovery for Large Transport Aircraft
Unsteady Aerodynamic Modeling in Rol for the NASA Generic Transport Model
Debris Aerodynamic Interactions during Uncontrolled Atmospheric Reentry
Gust Response Sensitivity Characteristics of Very Flexible Aircraft
Atmospheric Data System Sensor Placement Optimization for Mars Entry, Descent, and Landing
Simulation Tool for Testing and Validating UAV Autopilots in Wind Gust Environments
Flight Performance Issues of Electric Aircraft
Analysis of APC Characteristics of Control Mode Switching Induced by Active Side Stick
Effect Of Jump Strut Nose Landing Gear In Preliminary Design Of Aircraft
Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System
A Conceptual Study of Airfoil Performance Enhancement Using CFD
Bifurcation Analysis of the Generic Transport Model with a View to Upset Recovery
Method for Analyzing The Influence of Random Factors in Carrier Launching
Real-Time Frequency Response Estimation Using Multi-Sine Inputs and Recursive Fourier Transform
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
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
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
Continuous Differentiation of Complex Systems Applied to a Hypersonic Vehicle
Store Separation Equations of Motion