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Flugmechanik
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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
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
Use of Micro Spoilers for Control of Finned Projectiles
Modeling & Simulating Aircraft Stability & Control - SimSAC Project
Influence of Wing Flexibility on the Stability of Flapping Flight
Longitudinal Stability Analysis of a Jet-Powered Wingsuit
Benefits of Autonomous Morphing Aircraft in Loiter and Attack Missions
Reduced-Order Modeling of Hypersonic Vehicle Unsteady Aerodynamics
Transport Aircraft System Identification Using Roll and Yaw Oscillatory Wind Tunnel Data
Concurrent Learning Enabled Adaptive Limit Detection for Active Pilot Cueing
Hypersonic Vehicle Flight Dynamics with Coupled Aerodynamic and Reduced-Order Propulsive Models
On the Solution of Bilevel Optimal Control Problems to Increase the Fairness in Air Races
From Geometry to CFD Grids - An Automated Approach for Conceptual Design
Identification of a Robotic Samara Aerodynamic/Multi-Body Dynamic Model
Real-Time Aerodynamic Parameter Estimation Without Air Flow Angle Measurements
Real-Time Aerodynamic Parameter Estimation without Air Flow Angle Measurements
Aircraft Volterra Parameter-Varying Modeling Approach
System Identification of an Unmanned Aerial Vehicle with Hingeless Control Effectors
Flight Mechanics of a Novel Guided Spin-Stabilized Projectile Concept
Performance Characteristics of an Autonomous Airdrop System in Realistic Wind Environments
Control of a Stochastic Model of an Aeroelastic Micro Air Vehicle in Turbulence (AIAA 2013-4983)
Effects of Periodic Flight Trajectory on Endurance of a Remotely Piloted Aircraft (AIAA 2013-5163)
Flight Stability and Control of Articulated Wing Aircraft (AIAA 2013-4982)
Parameter Identification Technique based on Lyapunov Stability (AIAA 2013-4750)
Trajectory Control of Very Flexible Aircraft with Gust Disturbance (AIAA 2013-4745)
Flight Performance Feasibility Studies for the Max Launch Abort System (AIAA 2013-4685)
Nano-Satellite Deorbit by Bare Electrodynamic Tether (AIAA 2013-4683)
Statistical Impact Prediction of Decaying Objects (AIAA 2013-4682)
Towards the Design of a Pilot-induced-oscillation Detection and Mitigation Scheme (AIAA 2013-4605)
Time-Accurate Computations for Rapid Generation of Missile Aerodynamics