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Flugmechanik
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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
Longitudinal Flight Dynamics of Bio-Inspired Ornithopter Considering Fluid-Structure Interaction
Modeling of Nonlinear Flexible Aircraft Dynamics Including Free-Wake Effects
Attitude Control Augmentation Using Wing Load Sensing - A Biologically Motivated Strategy
Parametric Studies on UAV Flying Qualities
Orbital Dynamics Characteristics of a QB50 CubeSat Performing Atmospheric Reentry
Conceptual Flexible Aircraft Model for Modeling, Analysis and Control Studies
System Identification of a Quadrotor Micro Air Vehicle
Flight Stability of Asymmetric Projectiles with Control Mechanisms
Preliminary Design of Three-Dimensional Flapping Wings from a Wake-Only Energetics Model
Analytical Criterion for Aircraft Spin Susceptibility
Pitch Guidance Optimization for the Orion Ascent Abort Flight Tests
Autonomous VTOL Joined Wing UAV (AIAA 2013-5087)
LPV Aeroservoelastic Control using the LPVTools Toolbox (AIAA 2013-4742)
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
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
Experimental Study of Gust Effects on Micro Air Vehicles
Tethered Aerostat Modeling Using an Efficient Recursive Rigid Body Dynamics Approach
A UAV Model Parameter Identification Method
Some Applications of a Panel Method to Aerodynamic Modeling of Missiles
System Identification of an Ornithopter Aerodynamics Model