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Flugmechanik
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Hypersonic Vehicle Flight Dynamics with Coupled Aerodynamic and Reduced-Order Propulsive Models
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
L~1 Adaptive Control of Flexible Aircraft: Preliminary Results
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
Engine integration based on multi-disciplinary optimisation technique
Modeling and control of lift offset coaxial and tiltrotor rotorcraft
Wind-Shear Endurance Capability for Powered-Lift Aircraft
A New Flying Qualities Criterion for Flying Wings
Simulated Rarefield Aerodynamics of the Magellan Spacecraft During Aerobraking
Wind-Tunnel Investigation of Wind-Shear Effect on Turning Flight
Effect of Rotary Atmospheric Gusts on Fighter Airplane
Minimum-Fuel Trajectories for Hypersonic Vehicles with Aeropropulsive Interactions
Agricultural Tractor Tire Dynamic Indices
Aircraft with Single Axis Aerodynamically Deployed Wings
A Method of Wind Shear Detection for Powered-Lift STOL Aircraft
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
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Effect of an active high-lift system failure during landing approaches
An Automated Real-Time Spacecraft Navigation System
Thermal Snap of Satellite Solar Panels
A Method of Ground Resonance Testing for Helicopters
Air-bearing facility for the simulation of spin-stabilized satellites
Nonlinear Fuzzy Hybrid Control of Spacecraft
Eine Methode zur Analyse der Dynamik von räumlichen Landeklappenmechanismen in Fehlerfällen
Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
Compound Helicopter Optimum Design Based on Genetic Algorithm
Optimal approach minimizing aircraft noise and fuel consumption
Three-axis fluidic/electronic automatic flight control system - flight test report
Experimentelle und numerische Bestimmung der dynamischen Derivative
Stability of hingeless rotor blades in hover with pitch-link flexibility