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Flugmechanik
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SFB 880: fundamentals of high lift for future commercial aircraft
Engine integration based on multi-disciplinary optimisation technique
Optimal control : workshop, Universität Greifswald, 1.-3. Oktober 2002
Modeling and control of lift offset coaxial and tiltrotor rotorcraft
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
Effect of an active high-lift system failure during landing approaches
Analysis of trimmable conditions for a civil aircraft with active high-lift system
Aerodynamics and Structural Mechanics of Flapping Flight with Elastic and Stiff Wings
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
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
Addressing today's aeromechanic questions by industrial answers
Studies of trims, stability, controllability, and some flying qualities of a tandem rotor helicopter
Unmanned aerial vehicle aerodynamic model identification from a racetrack manoeuvre
Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
Flight controller design using multivariable loop shaping
Method for identification of non-linear multi-degree-of-freedom systems
Development of a new model with lumped elements for simulation of tethered systems
Navigation in the vicinity of a comet
The aeroelastic behaviour of a missile control fin with a pneumatic actuation system
The performance of CLOS missile systems against weaving targets
Helicopter flight control design: multivariable methods and design issues
The flight dynamics of an unstable unmanned aircraft
A reconfiguration algorithm for real-time aircraft flight control systems
An investigation into the phenomenon of helicopter blade sailing
Intelligent flight control systems
An analytical redundancy scheme for an automatic flight control system
Aerospace vehicle modelling requirements for high bandwidth flight control
Dynamics of a spinning spacecraft containing liquid propellant
Proof-mass actuator control of shuttle based astromast
Advanced control of high performance rotorcraft