Flow control for aircraft performance enhancements - Overview of airbus - University cooperation
Flight dynamics principles : a linear systems approach to aircraft stability and control
Flight dynamics principles : a linear systems approach to aircraft stability and control
Flight dynamics principles : [a linear systems approach to aircraft stability and control]
Flight dynamics principles : a linear systems approach to aircraft stability and control
A centrifugal force actuated variable span morphing helicopter rotor
Development of an attitude guidance and control system for the Thunderstar suborbital spacecraft
Stability and control analysis of the slowed-rotor compound helicopter configuration
Design and testing of an autorotative payload delivery system
Flight dynamic principles : a linear systems approach to aircraft stability and control
Morphing aircraft options at micro scale based on smart structural solutions
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
A multi-body approach for modelling manoeuvring aeroelastic aircraft during preliminary design
Parameter identification by free-flight wind tunnel tests
Velocity tracking control of a four-rotor mini helicopter
Main rotor-tail rotor interaction and its implications for helicopter directional control
From the test benches to the first prototype of the muFly micro helicopter
The effect of simulator motion on pilot control behaviour for agile and inert helicopter dynamics
Investigation on rotor blade-wake interaction noise in descent flight conditions
Genetic optimizations of EC-135 noise abatement flight procedures using an aeroacoustic database
A review of rotorcraft wake modeling methods for flight dynamics applications