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Flugmechanik
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Experimental Model Based Robust Aeroservoelastic Control for the S4T Wind-Tunnel Model
Stability Enhancement of a Transonic Wing Using a Simple Passive Attachment
Application of Structural Load Feedback in Flight Control
Suppression of Bending-Torsion Flutter in Accelerated Flight with Aero-Servo-Viscoelastic Controls
Controller and Aeroelasticity Analysis for a Morphing Wing
A New System Identification Method Using Short Duration Flight Test Inputs
Aircraft System Identification using Pseudospectral Parameter Optimization with Adaptive Nodes
High-fidelity Modeling and Simulation of Flutter/LCO for All-movable Horizontal Tail with Free-play
Unsteady Aeroelasticity of Generic Transport Model
Mixed Newtonian-Lagrangian Approach for the Analysis of Flexible Aircraft Dynamics
Development of a Simulation Environment to Support Aircraft Health Management Education
Verification of a Flying Wing Handling Qualities Analysis by means of In-Flight Simulation
Projectile Monte-Carlo Trajectory Analysis Using a Graphics Processing Unit
Solution methods for variational problems of low thrust space flight mechanics
Flight Test Maneuvers For Efficient Aerodynamic Modeling
Derivation and Analysis of the Equations of Motion for a Ducted Fan UAV
On the Applicability of an Unsteady Aerodynamic ROM to the Transonic Flight Regime
System Identification Applied to Dynamic CFD Simulation and Wind Tunnel Data
Ares I-X Range Safety Trajectory Analyses and Independent Validation and Verification
Flight Dynamics Modeling for a Small-Scale Flybarless Helicopter UAV
Estimation of Aircraft States and Wind Exposure
Envelopes for Flight Through Stochastic Gusts
Model-Based Strategies for Modern Flight Test
Concept of a Predictive Ship Helicopter Operational Limitations Analysis Tool
First Stage Solid Propellant Multiply Debris Thermal Analysis
Power Frequency - A New Metric for Analyzing Pilot-in-the-Loop Flying Tasks
Modeling and Flight Testing of the Longitudinal Dynamics of an Inflatable Wing UAV
Aerodynamic and Thrust Force Modeling for a Propulsion Assisted Control Aircraft Test Bed
Fin Mixing Optimization to Minimize Control Coupling Effects
Smart Projectile State Estimation Using Evidence Theory
Modeling, Stability Analysis and Simulation of a Stratosphere Hybrid Tethered Platform
Atmospheric flight mechanics / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Atmospheric flight mechanics / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Optimization of Flap-Bounding Flight
Real-Time Frequency Response Estimation from Flight Data
Data Gathering and Preliminary Results of the System Identification of a Flexible Aircraft Model
Determination of Sweet Spot for Trailing Aircraft in Formation Flight
Approach Trajectory Optimization including a Tunnel Track Constraint