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Flugmechanik
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Energy Harvesting Mechanisms for UAV Flight by Dynamic Soaring (AIAA 2013-4841)
Stability of a Mechanically Deployed Aerodynamic Decelerator (AIAA 2013-4602)
Analytical Investigation of Transport Aircraft Handling Qualities (AIAA 2013-4505)
Validating Uncertain Aircraft Simulation Models Using Flight Test Data (AIAA 2013-4984)
Dynamic Soaring of Albatrosses over Land (AIAA 2013-4842)
Parameter Estimation of Highly Unstable Aircraft Assuming Nonlinear Errors (AIAA 2013-4751)
Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations (AIAA 2013-4688)
Compendium of Flight Mechanics Formulae Applied to Hypersonic Gliders (AIAA 2013-4609)
Optimizing the Forces and Propulsive Efficiency in Bird-Scale Flapping Flight (AIAA 2013-4916)
Identification Of A Nonlinear Grey-Box Helicopter UAV Model (AIAA 2013-4847)
System Identification and Modal Extraction from Response Data (AIAA 2013-4919)
A Simple, Correct Pedagogical Presentation of Airplane Longitudinal Dynamics (AIAA 2013-4740)
Effect of Manipulator Feel System Characteristics on HQ of Aeroelastic Aircraft (AIAA 2013-4507)
ACS3 - Flight Dynamics for A Solar Sail Technology Demonstration Mission
Fused Reality for Enhanced Flight Test Capabilities (AIAA 2013-5162)
The Gulfstream G650 Flight Test Accident: Lessons Learned (AIAA 2013-5085)
Control Synthesis for Virtually Changing Wing Stiffness (AIAA 2013-4845)
Engine Limit Detection and Avoidance for Helicopters with Multiple Limits (AIAA 2013-4689)
Unique Range Performance Properties of Electric Aircraft (AIAA 2013-5088)
An Overview of NASA's SubsoniC Research Aircraft Testbed (SCRAT) (AIAA 2013-5083)
Aircraft Design Using Constrained Bifurcation and Continuation Method (AIAA 2013-5079)
Analysis of Modeling Techniques for Low-Cost Actuators (AIAA 2013-4846)
Flight Mechanics of Ram-Scram Transition (AIAA 2013-4687)
Investigation of a Flutter Exciter for Aircraft Flight Testing Using Unstructured Overset Grids
Evaluation of Multi-body Parafoil Dynamics Using Distributed Miniature Wireless Sensors
A Method for Optimizing Launch Vehicle Aero-Assist Including Path Optimization
Experiments on Free-to-Pivot Hover Motions of Multi-hinged Flat Plates
Characterisation of wind tunnel observed, large-amplitude pitch limit-cycles
Use of Flexible Body Coupled Loads in Assessment of Day of Launch Flight Loads
Use of Smoothed Measured Winds to Predict and Assess Launch Environments
UAV Flight Control Using Flow Control Actuators
Gust Load Alleviation Control for Very Flexible Aircraft
Validating the Multidimensional Spline Based Global Aerodynamic Model for the Cessna Citation II
Range Extension Of An Air-to-air Engagement By Offline Trajectory Optimization
Linear Parameter Varying Control for the X-53 Active Aeroelastic Wing
F-22 Raptor GBU-39 Separation Test Results