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Flugmechanik
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On the Solution of Bilevel Optimal Control Problems to Increase the Fairness in Air Races
Autonomous VTOL Joined Wing UAV (AIAA 2013-5087)
LPV Aeroservoelastic Control using the LPVTools Toolbox (AIAA 2013-4742)
F-22 Raptor GBU-39 Separation Test Results
Entry Guidance for the 2011 Mars Science Laboratory Mission
Ares I-X Best Estimated Trajectory and Comparison with Preflight Predictions
Flight Test of Orthogonal Square Wave Inputs for Hybrid-Wing-Body Parameter Estimation
Near Real-time Parameter Estimation in the C-12C
ACS3 - Flight Dynamics for A Solar Sail Technology Demonstration Mission
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
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)
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
Flight Tests, Performances and Flight Certification of a Twin-Engine Light Aircraft
Joined Wings Thrust Vectored UAV Flight Envelope
Aeroelastic Modeling and Adaptive Control of GTM
High Angle of Attack Model Identification Without Air Flow Angle Measurements (AIAA 2013-4980)
Assessment of Tabular Models Using CFD (AIAA 2013-4978)