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Flugmechanik
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keywords:("Flugmechanik")
Micro-Electromechanical Flying Insects - State of the Art
A Framework for Optimal Control Allocation with Structural Load Constraints
Estimation of Separation Aerodynamics Using Photogrammetric Data
Modeling Propeller Aerodynamics and Slipstream Effects on Small UAVs in Realtime
Performance and Stability of an Agile Tail-less MAV with Flexible Articulated Wings
Low Order Turbulence Modeling Methods for MAVs Flight Environment
Investigating Nonlinear Control Architecture Options for Aerial Refueling
Computational Analysis of the Bow Wave Effect in Air-to-Air Refueling
Rapid Entry Corridor Trajectory Optimization for Conceptual Design
Covariance Function Realization Algorithms for AeroElastic Dynamic Modeling
Identification and Validation of a F/A-18 Model Using Neural Networks
IRVE-II Post-Flight Trajectory Reconstruction
USNA/NAVAIR Cooperative Program in Store Separation
Robust Adaptive Control of a General Aviation Aircraft
Investigation of Maximum Range Cruise Flight for B787
Catastrophic Yaw Prevention for Cruciform Tailed Missiles
Comprehensive Characterization of Airship Response to Wind and Time Varying Mass
Aeroservoelastic Modeling of a Generic Transport Model
Dynamics, stability, and control analyses of flapping wing micro-air vehicles
Autonomous VTOL Joined Wing UAV (AIAA 2013-5087)
LPV Aeroservoelastic Control using the LPVTools Toolbox (AIAA 2013-4742)
High Angle of Attack Model Identification Without Air Flow Angle Measurements (AIAA 2013-4980)
Assessment of Tabular Models Using CFD (AIAA 2013-4978)
Evaluation of Piloted Inputs for Onboard Frequency Response Estimation (AIAA 2013-4921)
Virtual Deformation Control of the X-56A Model with Simulated Fiber Optic Sensors (AIAA 2013-4844)
A Rapid Aerodynamic Prediction Method for Simulation of Post-Stall Flight Dynamics
Structural Feedback for Enhanced MAV Flight
Modeling of Bow Wave Effect in Aerial Refueling
Methodological Remarks on CPG-Based Control of Flapping Flight
Nonlinearity Index Theory for Flight Mechanics Applications
Optimal Input and Output Blending for Adaptive Suppression of Adverse Aeroservoelastic Dynamics
Time-Accurate Computations for Rapid Generation of Missile Aerodynamics
Virtual Aircraft Design and Control of TransCruiser - A Canard Configuration
A Wake-Only Energetics Model for Preliminary Design of Biologically Inspired Micro Air Vehicles