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Flugmechanik
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keywords:("Flugmechanik")
Hypersonic Vehicle Flight Dynamics with Coupled Aerodynamic and Reduced-Order Propulsive Models
L~1 Adaptive Control of Flexible Aircraft: Preliminary Results
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
Joined Wings Thrust Vectored UAV Flight Envelope
Flight Mechanics of a Tailless Articulated Wing Aircraft
SFB 880: fundamentals of high lift for future commercial aircraft
Optimal control : workshop, Universität Greifswald, 1.-3. Oktober 2002
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
Modeling and control of lift offset coaxial and tiltrotor rotorcraft
Simulated Rarefield Aerodynamics of the Magellan Spacecraft During Aerobraking
Wind-Tunnel Investigation of Wind-Shear Effect on Turning Flight
Engine integration based on multi-disciplinary optimisation technique
Wind-Shear Endurance Capability for Powered-Lift Aircraft
Effect of Rotary Atmospheric Gusts on Fighter Airplane
A New Flying Qualities Criterion for Flying Wings
Minimum-Fuel Trajectories for Hypersonic Vehicles with Aeropropulsive Interactions
Aircraft with Single Axis Aerodynamically Deployed Wings
A Method of Wind Shear Detection for Powered-Lift STOL Aircraft
Agricultural Tractor Tire Dynamic Indices
Aerodynamics and Structural Mechanics of Flapping Flight with Elastic and Stiff Wings
Mission Performance Measures for Spacecraft Formation Flying
Analysis of trimmable conditions for a civil aircraft with active high-lift system
Thermal Snap of Satellite Solar Panels
Effect of an active high-lift system failure during landing approaches
An Automated Real-Time Spacecraft Navigation System
Eine Methode zur Analyse der Dynamik von räumlichen Landeklappenmechanismen in Fehlerfällen
Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
Nonlinear Fuzzy Hybrid Control of Spacecraft
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Air-bearing facility for the simulation of spin-stabilized satellites
Compound Helicopter Optimum Design Based on Genetic Algorithm
Three-axis fluidic/electronic automatic flight control system - flight test report
A Method of Ground Resonance Testing for Helicopters
Stability of hingeless rotor blades in hover with pitch-link flexibility
Addressing today's aeromechanic questions by industrial answers
Experimentelle und numerische Bestimmung der dynamischen Derivative
Optimal approach minimizing aircraft noise and fuel consumption