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Flugmechanik
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keywords:("Flugmechanik")
AB levitator and electricity storage
About the Use of Vortex Generators to Improve Aircraft Aerodynamics
Accuracy Modeling for Short-Arc Determination of Low Earth Orbits
A cooperative approach to multi-level multi-disciplinary aircraft optimization
Actively translating a rear diffuser device for the aerodynamic drag reduction of a passenger car
Advanced flow simulation methods in aircraft design
Aeroacoustic Characteristics of a Quadcopter Impeller in Vertical Take-Off and Landing Mode
Aerodynamic calculation of unmanned aircraft
Aerodynamic characteristics of a wrap-around fin rocket
Aerodynamic Design and Performance Research of Racing Cars with Adaptive Control of Attitude
Aerodynamic design optimization of rear body shapes of a sedan for drag reduction
Aerodynamic investigation on tiltable endplate for WIG craft
Aerodynamic modellers take off with design software
Aerodynamic parameter estimation using adaptive unscented Kalman filter
Aerodynamic performance of Parastoo UAV
Aerodynamic performance of thin wings at low Reynolds numbers
Aerodynamic study of a generic car model with wheels and underbody diffuser
Aeroelasticity consideration of supersonic vehicle using closed form analytical aerodynamic model
Aero-mechanical design of high-lift systems
Aircraft Control and Simulation
Aircraft design using a variable density model
A model governing the stall characteristics of an isolated axial compressor rotor
A Modernized Approach to Meet Diversified Earth Observing System (EOS) AM-1 Mission Requirements
Analyses on ducted tail rotor and airfoil aerodynamic characteristics with CFD
Analysis of flight dynamics for large-scale morphing aircraft
An Approach to the Design and Implementation of Spacecraft Attitude Control Systems
An Autonomous Navigator for LEO Satellites
An Efficient Algorithm for Spacecraft Attitude Determination With Optical Sensors
An efficient method for solution of inverse dynamics of Stewart platform
An Efficient On-Board Orbit Propagator/Estimator for LEO Missions
A new method for predicting rotor wake geometries and downwash velocity field
An integrated design approach for low noise exposing high-lift devices
A nonlinear inverse simulation technique applied to coaxial rotor helicopter maneuvers
Approximate controller design for singularly perturbed aircraft systems
A review of conventional and synergistic systems for small satellites
A Robust Star Acquisition Algorithm for the Wide-Field Infrared Explorer
A study of solar-powered, high-altitude unmanned aerial vehicles
A Transition Matrix Approach to the Davenport Gyro Calibration Scheme
Attitude Commands Avoiding Bright Objects and Maintaining Communication With Ground Station
Attitude Propagation Using Non-Singular Canonical Variables
Automobile aerodynamics influenced by airfoil-shaped rear wing
Autonomous Star Identification Using Fuzzy Neural Logic Network
BAE Systems flies world's first flapless air vehicle
BAE Systems success in flapless flight