The T-Wing tail-sitter unmanned air vehicle: From design concept to research flight vehicle
The stability and control characteristics of the neutrally bouyant non-rigid airship
The Mass Growth Factor – Snowball Effects in Aircraft Design
The Mass Growth Factor – Snowball Effects in Aircraft Design
The implementation of an autonomous helicopter testbed
The effect of simulator motion on pilot control behaviour for agile and inert helicopter dynamics
The effect of airframe aerodynamics on V-22 rotor loads
The Dolphin 6075: an helicopter dedicated to flight test research
TEDAS II - High speed data acquisition, storage and distribution
Technische Entwicklung von Bodeneffektfahrzeugen TEBEFPhase 2
System identification modeling of a small-scale unmanned rotorcraft for flight control design