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Flugmechanik
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keywords:("Flugmechanik")
Real-Time Onboard Global Nonlinear Aerodynamic Modeling from Flight Data (AIAA 2014-2554)
Parachute Dynamic Stability and the Effects of Apparent Inertia (AIAA 2014-2390)
F-35A High Angle-of-Attack Testing (AIAA 2014-2057)
Trimming Mass-Actuated Airplane in Turns with Zero Side Slip Angle (AIAA 2014-0192)
Dynamic Analysis of the Meridian Unmanned Aerial Vehicle (AIAA 2014-0191)
Pressure/Temperature Measurement of a Free-Flight Object by PSP/TSP (AIAA 2014-2542)
Implementation of a Trajectory Prediction Function for Trajectory Based Operations (AIAA 2014-2198)
Aeroelastic Optimization Study Based on the X-56A Model (AIAA 2014-2052)
Optimization of a Martian Aero-Gravity Assist (AIAA 2014-1232)
Flight Testing of a Subscale Aeroservoelastic Aircraft (AIAA 2014-0032)
Computational Studies for Pressure Sensor Placement on a Fish-Inspired UUV (AIAA 2014-2813)
Simultaneous Tracking of Multiple Ground Targets from a Single Multirotor UAV (AIAA 2014-2670)
An Autonomous Recovery System for High Altitude Payloads by Using a Parafoil (AIAA 2014-2555)
Simulation of a Variety of Wings using a Reynolds Stress Model (AIAA 2014-2192)
Limit Circular Motion of Spinning Projectiles Induced by Backlash of Actuators (AIAA 2014-0886)
Modified Study of Trail Aircraft Trim Effect on Sweet Spot in Formation Flight (AIAA 2014-0541)
Supersonic Propulsive Divert Maneuvers for Future Robotic and Human Mars Missions (AIAA 2014-0386)
Trajectory Analysis of Basket Engagement during Aerial Refueling (AIAA 2014-0190)
Aerodynamic Parameter Estimation of a Missile without Wind Angle Measurements (AIAA 2014-2557)
Feasible area coverage of a hurricane using micro-aerial vehicles (AIAA 2014-0894)
Numerical analysis for an aerial deployment motion of a folded-wing airplane (AIAA 2014-0383)
Real-Time Parameter Estimation Using Output Error (AIAA 2014-2556)
Toward a Flying Qualities Standard for Unmanned Aircraft (AIAA 2014-2194)
Fly-by-Feel Sensing and Control: Aeroservoelasticity (AIAA 2014-2189)
Assessing the Impact of Aerodynamic Modelling on Manoeuvring Aircraft (AIAA 2014-0732)
Lower Stratospheric Deployment Testing of a Ram-Air Parafoil System (AIAA 2014-0193)
Solution of Lambert's Theorem with Additional Terminal Constraints (AIAA 2014-2543)
Advanced Optical Sensor Technology: Launch Vehicle and Spacecraft Applications (AIAA 2014-2540)
Time-Varying Entry Heating Profile Replication with a Rotating Arc Jet Test Article (AIAA 2014-2384)