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Flugmechanik
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keywords:("Flugmechanik")
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
Continuous Differentiation of Complex Systems Applied to a Hypersonic Vehicle
Store Separation Equations of Motion
Aerodynamic Parameter Identification for Symmetric Projectiles: An Improved Gradient Based Method
A Two-Stage Method for the Parametric Identification of Scale-Model Helicopter Dynamics
Simulation of Aircraft Encounters with Perturbed Vortices Considering Unsteady Aerodynamic Effects
Modeling and Detection of Ice Particle Accretion in Aircraft Engine Compression Systems
Trim Analysis of a Moving-mass Actuated Airplane
Bifurcation Behaviour of a Flapping Wing MAV in Longitudinal Flight
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
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
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
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