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Flugmechanik
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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
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
Trajectory-Based Loads for the Ares I-X Test Flight Vehicle
Modeling Interactions Between Flexible Flapping Wing Spars, Mechanisms, and Drive Motors
Adaptive Flutter Suppression for Aircraft Upset and Damage Conditions
Assessment of Helicopter Model Fidelity through Inverse Simulation
Affordable State Estimation Using Inertial Navigation Sensor Arrays
Method for Rapid Modelling of Missile Aerodynamics
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 theory and aerodynamics : a practical guide for operational safety
Helicopter aerodynamics / Ray Prouty ; Volume 3: Ray Prouty's Vertiflite Magazine columns 1990-2013
The Recovery of Energy from Leading- and Trailing-Edge Vortices in Tandem-Airfoil Configurations
Transonic Aeroelastic Stability Analysis Using a Kriging-Based Schur Complement Formulation
Parameter Varying Estimation Toolbox for Flutter Prediction
Aeroservoelastic Analysis of a Typical Business Jet Configuration Involving Nonlinear Actuators
Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation
System Identification of a COTS Autopilot System Using Flight Test Data
Specialized System Identification for Autonomous Parafoil and Payload Systems
Correlating Kinematics and Control Inputs on Small-Scale Helicopters
Controller Synthesis and Application to Hover-to-Cruise Transition Flight of a Tail Sitter UAV
Stability Analysis in Conceptual Design Using SDSA Tool
Modeling of Dynamic Loading of Morphing Wing Aircraft
Aerodynamic and Structural Measurement of the Aerostructures Test Wing for Flutter Testing
Effects of Wing Design on Aerodynamics of MAVs in Turbulent Flow
Flight Mechanics of a Tailless Articulated Wing Aircraft
Practical Aeroservoelasticity In-Flight Identification and Adaptive Control
Estimation of Projectile Aerodynamic Coefficients Using Coupled CFD/RBD Simulation Results