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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
A Method of Ground Resonance Testing for Helicopters
Air-bearing facility for the simulation of spin-stabilized satellites
Thermal Snap of Satellite Solar Panels
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